C USAGE AGREEMENT NUMBER REV MATERIAL USAGE AGREEMENT … MUA 1.pdf · c usage agreement number rev...

C USAGE AGREEMENT NUMBER REV MATERIAL USAGE AGREEMENT PAGE 1 OF 90 PROJECT:

PGBA-4 SYSTEM:

SUBSYSTEM:

ORIGINATOR: Alex Hoehn

ORGANIZATION/CONTRACTOR:

BioServe PART NUMBER(S): USING ASSEMBLY(S): ITEM DESCRIPTION: ISSUE:

PGBA-4 S/N –001 & -002

Double middeck locker replacement

MATERIAL DESIGNATION:

MANUFACTURER: SPECIFICATION: PROPOSED EFFECTIVITY:

BioServe

Flight 9A / STS-112 Flight 11A / STS-113

MATERIAL CODE: LOCATION: ENVIRONMENT THICKNESS: WEIGHT: EXPOSED

AREA: HABITABLE XXX PRESSURE

PSIA: TEMP, F: MEDIA:

NONHABITABLE APPLICATION: THIS MUA PROVIDES CERTIFICATION OF THE FOLLOWING HARDWARE PER THE PROVISIONS AND RESTRICTIONS OF NHB 1700.7. FLAMMABILITY ACCEPTABLE PER CRITERIA FO NHB-8060.1 AND NSTS 22648; OUTGASSING ACCEPTABLE PER CRITERIA OF NHB-8060.1 TEST 1 AND NASA-STD-6001, TEST 7; STRESS CORROSION ITEMS REPORTED ARE ACCEPTABLE. RATIONALE: THIS CERTIFICATION IS BASED ON THE EVALUATION OF THE FINAL MATERIALS LIST AND THE FOLLOWING: PGBA MP-ER-001 SUBMITTAL ATTACHMENT 1: OFFGAS DATA ATTACHMENT 2: ENVIRONMENTAL COMPATIBILITY ATTAHCMENT 3: MATERIALS USAGE SUMMARY FOR STS-112 / ISS.9A ATTACHMENT 4: MATERIALS USAGE SUMMARY BY TBE FOR STS-83 STRESS CORROSION CRACKING ASSESSMENT TOXICITY ASSESSMENT FLAMMABILITY ASSESSMENT ATTACHMENT 5: MATERIALS USAGE SUMMARY BY MCDONNELL DOUGLAS FOR STS-77 PGBA IS A MIDDECK PAYLOAD AND THEREFORE REQUIRES NO THERMAL VACUUM STABILITY TESTING. THERE ARE NO OPEN ITEMS.

MATERIAL USAGE AGREEMENT DISPOSITION CONTRACTOR M & P CONTRACTOR PROJECT

MGR. ISS PRIME M & P NASA M & P

MAEB Chairman

DATE APPROVE REJECT DEFER MEMO NO.:

EFFECTIVITY:

For clarifications, please contact: Alex Hoehn BioServe Space Technologies 303.492.5875

ORIGINATING CONTRACTOR:

SSP52000-PVP-ERP

H:\Verification-Submittals\PGBA\PVP-STS112-ISS9A\PGBA4-MP-ER-001-ISS9A-materials-parts-revB.doc 4/9/02 - 2:25 PM

DATA CERTIFICATION I hereby certify compliance with the verification requirements as specified in SSP 52000-IDD ERP, Issue C, dated 08/07/2001. I also certify the identified as-built hardware, per the current applicable Engineering Configuration List, was manufactured in accordance with the design drawings, parts list, applicable waivers, and deviations. All supporting data is valid, applicable, and complete. The data is maintained in our files and will be made available upon request. Payload VRDS Number Method Applicable

Document Rev. Date Completion Date

Summary (attach sheets as needed)

PGBA-4

S/N-01

and

S/N-02

MP-ER-001

A, T, I

PGBA4-MP-ER-001-ISS9A-materials-parts.doc Rev. B 12/03/2001

12/01/01

(w/o MIUL)

01/16/02 (added MIUL)

04/09/02

(updated MIUL)

PGBA-4 is the forth flight of PGBA with essentially no changes that would invalidate previous materials and parts assessments by McDonnell Douglas and Teledyne Brown Engineering. The MIUL has been updated as necessary for minor changes, and the impact of these changes has been assessed (see attached document). See attached document: PGBA4-MP-ER-001-ISS9A-material- and-parts.doc

09 April 200209 April 2002 Alex Hoehn, Ph.D. Associate Director Engineering - BioServe Space Technologies Campus Box 429 - Boulder CO 80309-0429, USA +1-303-492-5875 phone / +1-303-492-8883 fax email: mailto:[email protected] web: http://spot.colorado.edu/~hoehn/ http://www.colorado.edu/engineering/BioServe/

BioServe Space Technologies Payload Verification Page 1 of 24 Payload: PGBA4 Mission: ISS.9A Prepared by / Date: Alex Hoehn, 12/01/01 VRDS: MP-ER-001 Title: Materials and Parts Delivery type: 1st (L-9 months) File: PGBA4-MP-ER-001-ISS9A-materials -parts.doc

Method: A and T and I Hazard Report: STD-PGBA, PGBA-7, PGBA-11, PGBA-13

Table of Contents

Applicable Documents and Notes:....................................................................................................................................... 2 Materials and Parts Verification Requirement: ................................................................................................................. 2 Description of Verification Method:................................................................................................................................... 3 Required Verification Data / Submittal Dates:.................................................................................................................. 4 Description of Reverification Requirements:..................................................................................................................... 4

PGBA MP-ER-001 Submittal ................................................................................................................................................... 4 Summary of analysis and test reports .................................................................................................................................. 8 PGBA4 Submittal MP-ER-001 – item 3: ........................................................................................................................... 9

Attachment 1 – Offgas Data .................................................................................................................................................... 10 Attachment 2 – Environmental Compatibility...................................................................................................................... 12

LCD Screen:...................................................................................................................................................................... 12 Materials Compatibility of Exposed PGBA Components ......................................................................................... 12

Attachment 3 – Materials Usage Summary for STS-112 / ISS.9A................................................................................... 14 Summary ............................................................................................................................................................................ 15

Attachment 4 – Materials Usage Summary by Teledyne Brown Engineering for STS-83 (David Eze ll)................. 16 PGBA General Description................................................................................................................................................. 16 Stress Corrosion Cracking Assessment............................................................................................................................. 17 Toxicity Assessment ............................................................................................................................................................ 18 Flammability Assessment.................................................................................................................................................... 18

Shell Assembly (Double-Locker).................................................................................................................................. 18 Structure Faceplate........................................................................................................................................................... 18 Plant Chamber Structure ................................................................................................................................................. 18 Root Tray Assembly ........................................................................................................................................................ 18 Air Plenum and Blower................................................................................................................................................... 18 Plant Chamber Electronics.............................................................................................................................................. 18 Humidity Control System ............................................................................................................................................... 18 Temperature Control Electronics ................................................................................................................................... 18 Carbon Dioxide Removal System ................................................................................................................................. 18 Ethylene Removal System.............................................................................................................................................. 19 Water Containment System............................................................................................................................................ 19 Atmosphere Control System, .......................................................................................................................................... 19 Atmosphere Control Electron9ics.................................................................................................................................. 19 Nutrient delivery System................................................................................................................................................. 19 Video System .................................................................................................................................................................... 19 Light Box Assembly ........................................................................................................................................................ 19 Computer Assembly......................................................................................................................................................... 19 Power Assembly ............................................................................................................................................................... 19 Wire Harness..................................................................................................................................................................... 19

PGBA Picture ........................................................................................................................................................................ 20 Attachment 5 – Materials Usage Summary by McDonnell Douglas for STS-77. ......................................................... 22

PGBA4-MP-ER-001-ISS9A-materials-parts.doc PGBA on ISS.9A Page - 2

LIST OF FIGURES PAGE FIGURE 1. PGBA OVERVIEW 15 FIGURE 2. PGBA DOUBLE LOCKER AND PLANT CHAMBER ACCESS. 16 FIGURE 3. PGBA TRANSFER TO/FROM ISS 17 FIGURE 4. PGBA IN EXPRESS / PGBA MUFFLERS (ISS) 17 FIGURE 5. PGBA OPENED 20 FIGURE 6. PGBA INNER GUTS - SIDE VIEWS 20 FIGURE 7. PGBA INNER GUTS – BACK VIEW / CLAM SHELL 21 FIGURE 8. PGBA FACEPLATE ASSEMBLY 21

Applicable Documents and Notes: JSC SN-C-0005 MIL-HDBK-454 MIL-STD-810 MSFC-SPEC-250: total document MSFC-SPEC-522: total document MSFC-HDBK-527/JSC 09604: total document NASA-STD-6001: sec 4.1, 4.7, 4.15 NSTS 1700.7: par 208.3, 209.1, 209.1A, 209.1B, 209.3, 220.10 NSTS 1700.7, ISS Addendum: par 208.3, 209.1, 209.1A, 209.1B, 209.2B, 209.3, 220.10 NSTS 22648: total document SSP 30233: total document SSP 30573: sec 4.0 SSP 52000-IDD-ERP: par 5.3.1.5.2A, 5.3.1.5.2B, 5.3.1.5.2C, 10.1A, 10.1B, 13.1, 13.1.1, 13.1.2, 13.1.3, 13.1.4, 13.2, 13.3, 13.4, 14.1.1 SSP 52000-PAH-ERP: par 4.8.4 Note: The COCs are required to support/substantiate the Phase 3 Flight Safety Review Data Package for the

integrated EXPRESS Rack.

Materials and Parts Verification Requirement: 1. The materials and parts used in the design of the payload hardware must accurately reflect the as -built

hardware. (5.3.1.5.2) 2. Payloads which connect to ISS fluid systems shall use fluids that meet the requirements specified in SSP 30573.

(5.3.1.5.2A, 13.1) Payloads which connect to ISS fluid systems shall meet the fluid system cleanliness levels specified in SSP 30573. (5.3.1.5.2B, 13.1)

3. Surface Cleanliness - Payloads shall conform to Visibly Clean-Sensitive (VC-S) cleanliness requirements as specified in SN-C-0005. (10.1B) Payload design shall allow external surfaces to be cleaned with solvents and equipment available at the launch site (lint free cloths/swabs, isopropyl alcohol, demineralized water, etc.). Visibly clean “SENSITIVE” is the baseline level for all payloads. (10.1A)

4. Stress Corrosion Cracking - Metallic materials (especially those considered to be structure members, such as payload structures, support bracketry, and mounting hardware, and those whose failure could result in a critical or catastrophic hazard), which have a high resistance to SCC according to the criteria of MSFC-SPEC-522 shall be used preferentially. (13.1, 13.1.1) Note: All materials used in fracture-critical structures must have a documented audit trail that assures only materials specified by the drawing have been used. (13.4)

5. Materials Compatibility - The use of materials, chemicals, and fluids which could create a toxic or hazardous situation for the crew, or which could contribute to the deterioration of hardware in service, shall be given special consideration as to adequate containment and compatibility. (13.1, 13.1.2)

6. Flammability, Nonmetallic Materials - Payload materials shall be nonflammable or self-extinguishing per the test criteria of NHB 8060.1. (13.1, 13.1.3, 14.1.1)

7. Toxic Offgassing - All flight hardware located in habitable areas shall meet the toxicity offgassing acceptance requirements of NASA-STD-6001, Test 7. (13.1, 13.1.4)


8. Galvanic Corrosion - Payloads using ISS fluid systems/EXPRESS Rack fluid systems shall use internal materials that are compatible according to MSFC-SPEC-250, Table III, or that will not create a potential greater than 0.25 V with the ISS system internal materials due to a dissimilar metal couple. (5.3.1.5.2C, 13.2)

9. Fungus-Resistant Materials - Payloads that are intended to remain on-orbit for more than 1 year shall use fungus-resistant materials according to the requirements specified in SSP 30233, para. 4.2.10. (13.3)

Description of Verification Method: 1. Verify by inspection that the materials used in the design of the payload hardware accurately reflect the as -built

configuration. 2. Verify by test that all payloads, which connect to ISS fluid systems, use fluids that meet the physical and

chemical requirements specified in SSP 30573, Section 4. The verification shall be considered successful when the test results show the fluids used in the payloads comply with the physical and chemical requirements specified in SSP 30573. Verify by test the fluid systems cleanliness levels. The verification shall be considered successful when sampling tests per SSP 30573, Section 4 show that fluids in the fluid system hardware comply with cleanliness levels specified. Verify by analysis that all payload materials in contact with the fluid coolant are compatible with the fluid and do not support microbial growth, or that MUAs have been approved for the usage. An analysis shall be performed to determine the compatibility of the fluid coolant with the payload materials it contacts. The verification shall be considered successful when the analysis shows the payload materials in contact with the fluid coolant are compatible with the fluid coolant.

3. Verify by inspection that the payload exterior and accessible interior surfaces are in accordance with VC-S cleanliness requirements as specified in JSC SN-C-0005. An inspection of the cleanliness documentation shall be performed to show the exterior and accessible interior surfaces meet the VC-S requirements. The verification will be considered successful when the inspection shows the payload exterior and accessible interior surfaces meet the VC-S cleanliness requirements specified in JSC SN-C-0005. Verify by analysis that all payload equipment exterior and accessible interior surfaces are capable of being cleaned with solvents and equipment at the ISS launch sites and on-orbit. A compatibility analysis shall be performed to determine if the payload exterior and accessible interior surfaces can be cleaned with solvents and equipment at the ISS launch sites and on-orbit. The verification shall be considered successful when the analysis shows the payload exterior and accessible interior surfaces are capable of being cleaned with solvents and equipment at the ISS launch sites and on-orbit.

4. Verify by analysis that no stress corrosion susceptible materials per MSFC-SPEC-522 are used, or that Material Usage Agreements (MUA) have been approved for their use. The analysis shall compare the materials and parts list and the drawings with the materials listed in MSFC-SPEC-522. The verification shall be considered successful when the analysis shows that no stress corrosion susceptible materials per MSFC-SPEC-522 are used, or that MUAs have been approved for their use.

5. Verify by analysis or test that hazardous materials are compatible with their containment system materials of construction per the requirements of NSTS 1700.7, ISS Addendum, paragraphs 209.1a and 209.1b, and/or are compatible with their use environment. Verify by analysis or test that sample materials are compatible with their containment system. An acceptable test method is NASA-STD-6001, Test 15. Verify by analysis or test that the nominal/planned release of materials to the cabin does not constitute a hazard or could be detrimental to other materials in the cabin.

6. Verify by inspection that the materials used in the design of the payload hardware accurately reflect the as -built configuration. Verification of payload hardware flammability shall be by inspection. The inspection shall determine whether the payload materials either meet the flammability acceptance criteria of NASA-STD-6001 per the worst-case use conditions of NSTS 1700.7, ISS Addendum, or that sufficient justification documentation (such as MUAs) for flammable materials used in quantities as noted in NSTS 1700.7, ISS Addendum, has been presented and approved to allow their use. The verification shall be considered successful when the inspection shows that the payload materials are either nonflammable or self-extinguishing per NHB 8060.1, or that sufficient justification has been approved for their use.

7. Verification of toxic offgassing by payload hardware shall be by test. A test shall be conducted on all payload hardware per the conditions and criteria of NASA-STD-6001, Test 7, to determine the suitability of the payload nonmetallic materials and assembled articles used in crew compartment environments with respect to toxic offgassed products. The verification shall be considered successful when the test results show the payloads in habitable areas meet the toxic offgassing acceptance criteria of NASA-STD-6001, Test 7.


8. Verification of dissimilar metals compatibility shall be by inspection or analysis. The inspection shall compare the materials and parts list with the materials listed in MSFC-SPEC-250, Table III. Verification shall be considered successful when the inspection of the materials and parts list shows that the internal materials used in the integrated rack aqueous fluid systems are compatible according to the table specified. Analysis shall be performed on materials not listed in MSFC-SPEC-250, Table III. Verification shall be considered successful when the analysis of the materials shows that the internal materials used in the integrated rack aqueous fluid systems do not create a dissimilar metal couple greater than 0.25 V with the ISS aqueous fluid system.

9. Verify by inspection that payloads which are intended to remain on-orbit for more than 1-year uses materials that are non-nutrient per the requirements of SSP 30233, par 4.2.10. If a fungus-nutrient material must be used, verify by inspection that it is treated to prevent fungus growth, or that its usage satisfies the requirement. Inspection of design drawings and materials lists shall determine whether fungus-resistant materials have been used as required. Verification shall be considered successful when the inspection shows fungus-resistant materials are used as required.

Required Verification Data / Submittal Dates: 1. Certificate of Compliance (COC) with the requirements. The COC must include the concurrence of an ISS

Program-approved Materials and Processes organization (e.g., the Materials and Processes organizations of NASA field centers which participate in the Materials and Processes Intercenter Agreement) [submit L-4.5 months].

2. Analysis and test reports to support rack level analysis of nominal/planned release of materials [submit L-7 months].

3. Analysis and drawings to support rack-level analysis of flammability [submit L-7 months].

Description of Reverification Requirements: 1. On-orbit subrack payload changeout: Same as the “Description of Verification Requirement” identified above. 2. Payloads remaining on-orbit past the original period of certification of the safety features or inhibits must

perform a re -verification of the activities as identified in the “Description of the Verification Method” identified above. This is the reverification requirement for safety features as per NSTS 18798B, MA2-98-135. It covers not only items that are limited operating life items (i.e., batteries, seals, etc.) but also items such as micro-switches, PRVs, etc., that perform the safety control function for a payload hazard.

Required Reverification Data: 1, 2. Same as “Required Verification Data” identified above. Data Submittal Dates: L-6 months / L-9 months / L-9 months.

PGBA MP-ER-001 Submittal 1. Verify by inspection that the materials used in the design of the payload hardware accurately reflect the as-built

configuration.

The MIUL has been compared to the as-built hardware and accurately reflects the as-built status of the PGBA4 payload. PGBA has flown on three previous missions, STS-77, STS_83 and STS-94. The MIUL was originally prepared for STS-77, reviewed and approved for flight by McDonnell Douglas (Now Boeing Spacehab Huntsville). The MIUL was updated as needed for flight STS-83, submitted to TBE (Spacehab) for review, and approved for flight by TBE (David Ezell, TBE).

The MIUL was again updated for flight STS-112 (PGBA4 – this submittal). Minor changes include the replacement of power and data connectors with ‘like’ connectors using the EXPRESS pin arrangements (same materials), and replacement of various metallic components (non-fracture critical brass fittings were replaced with stainless steel parts of the same function). No new non-metallic materials were added.


2. Verify by test that all payloads, which connect to ISS fluid systems use fluids that meet the physical and chemical requirements specified in SSP 30573, Section 4. The verification shall be considered successful when the test results show the fluids used in the payloads comply with the physical and chemical requirements specified in SSP 30573.

N/A: The PGBA-04 payload does not connect to the ISS fluid system. PGBA contains its own internal water circulation system, which is NOT connected to ISS.

Verify by test the fluid systems cleanliness levels. The verification shall be considered successful when sampling tests per SSP 30573, Section 4 show that fluids in the fluid system hardware comply with cleanliness levels specified.

N/A: The PGBA-04 payload does not connect to the ISS fluid system. PGBA uses a 10% ethanol-water mixture. The ethanol is dissolved in the water coolant system, which is a proof and leak-tested, sealed, pressurized coolant circulation system. The use of alcohol in this application eliminates potential bacterial contamination, and acts as a gear pump lubricant. The use of alcohol in this sealed application is approved.

Verify by analysis that all payload materials in contact with the fluid coolant are compatible with the fluid and do not support microbial growth, or that MUAs have been approved for the usage. An analysis shall be performed to determine the compatibility of the fluid coolant with the payload materials it contacts. The verification shall be considered successful when the analysis shows the payload materials in contact with the fluid coolant are compatible with the fluid coolant.

N/A: The PGBA-04 payload does not connect to the ISS fluid system. See above.

3. Verify by inspection that the payload exterior and accessible interior surfaces are in accordance with VC-S cleanliness requirements as specified in JSC SN-C-0005. An inspection of the cleanliness documentation shall be performed to show the exterior and accessible interior surfaces meet the VC-S requirements. The verification will be considered successful when the inspection shows the payload exterior and accessible interior surfaces meet the VC-S cleanliness requirements specified in JSC SN-C-0005. Verify by analysis that all payload equipment exterior and accessible interior surfaces are capable of being cleaned with solvents and equipment at the ISS launch sites and on-orbit. A compatibility analysis shall be performed to determine if the payload exterior and accessible interior surfaces can be cleaned with solvents and equipment at the ISS launch sites and on-orbit. The verification shall be considered successful when the analysis shows the payload exterior and accessible interior surfaces are capable of being cleaned with solvents and equipment at the ISS launch sites and on-orbit.

The PGBA-04 payload will be cleaned prior to shipment to KSC, and will be re-cleaned prior to handover. At that point, a certificate of cleanliness will be signed and provided at handover. All surfaces are cleaned using approved cleaning agents, provided by Hangar-L or SSPF (typical citrus cleaner, and historically isopropyl alcohol). “KSC ISS-Utilization” personnel (a.k.a. Jeannie Ruiz and colleagues) ALWAYS re-clean, and re-verify cleanliness at handover, prior to moving the payload to the launch pad.

All PGBA accessible exterior and internal surfaces are compatible with the listed and approved cleaning agents. The materials compatibility analysis is on file. Most surfaces are metal (anodized aluminum or steel), with some polycarbonate surfaces (light box, plant chamber box, LCD screen frame, LED lenses and lens covers / holders), and Teflon-insulated wire harnesses. These non-metallic surfaces are all compatible with the approved and customary solvents. See attachment 2 – Materials Compatibility Analysis for PGBA materials exposed to cleaning agents or chemicals in potential contact during laboratory work at Hangar L, SSPF or during payload integration at the pad.

NOTE: Critical items include Polycarbonate (LCD screen frame / cover, lamp box lid, plant chamber lid).


4. Verify by analysis that no stress corrosion susceptible materials per MSFC-SPEC-522 are used, or that Material Usage Agreements (MUA) have been approved for their use. The analysis shall compare the materials and parts list and the drawings with the materials listed in MSFC-SPEC-522. The verification shall be considered successful when the analysis shows that no stress corrosion susceptible materials per MSFC-SPEC-522 are used, or that MUAs have been approved for their use.

The stress corrosion assessment is listed in the updated MIUL for PGBA-04 (ISS.12A). There are only A-rated materials in the PGBA-04 fluid system (pressurized system). All safety-critical structures (PGBA locker replacement shell, mounting brackets, faceplate, pressurized systems) use A-rated materials. There are some B-rated materials in non-critical (neither structural nor pressurized components) applications. These materials were previously approved for flight in an independent review by McDonnell Douglas (STS-77) and Teledyne Brown Engineering (STS-83, STS-94).

5. Verify by analysis or test that hazardous materials are compatible with their containment system materials of construction per the requirements of NSTS 1700.7, ISS Addendum, paragraphs 209.1a and 209.1b, and/or are compatible with their use environment.

Materials compatibility evaluations are performed on a mission-specific assessment by analysis and test. The compatibility report is on file (Carla Goulart, BioServe). All primary, secondary and tertiary levels of containment (as applicable) are compatible with the material to be contained. This verification is primarily controlled by PGBA-unique and PGBA generic hazard reports, and verified with the PSRP and Payload Safety Engineer assigned to PGBA by the PSRP. This verification item 5 in MP-ER-001 appears redundant, and should be eliminated, as its primary control is not EXPRESS, but PGBA hazard reports.

Verify by analysis or test that sample materials are compatible with their containment system. An acceptable test method is NASA-STD-6001, Test 15.

See above. All materials of all levels of containment are tested or analyzed. These types of analysis have been performed on 21 previous missions by BioServe, and all data is on file. Adequate materials compatibility has been documented for all missions. Tests and analysis include exposure tests to 1.5 times the planned mission duration per approved PGBA hazard reports.

Verify by analysis or test that the nominal/planned release of materials to the cabin does not constitute a hazard or could be detrimental to other materials in the cabin.

N/A: there is no nominal release of materials from the PGBA payload. PGBA is a greenhouse, growing plants. As such, PGBA utilizes ISS / NSTS cabin air as an oxygen and carbon dioxide source, and produces oxygen (day) and carbon dioxide (night) in VERY SMALL QUANTITIES in return. The metabolic rate of these processes is very low given the small growth area and light levels. The release of oxygen or carbon dioxide is very small (1/100 to 1/1000 of an astronaut), and negligible when compared to the respiration rate of a human being. The release of gaseous oxygen, carbon dioxide and air humidity at cabin atmosphere levels (21% O2, < <0.1% CO2, <80% r.H.) is not a hazard.


6. Verify by inspection that the materials used in the design of the payload hardware accurately reflect the as-built configuration. Verification of payload hardware flammability shall be by inspection. The inspection shall determine whether the payload materials either meet the flammability acceptance criteria of NASA-STD-6001 per the worst-case use conditions of NSTS 1700.7, ISS Addendum, or that sufficient justification documentation (such as MUAs) for flammable materials used in quantities as noted in NSTS 1700.7, ISS Addendum, has been presented and approved to allow their use. The verification shall be considered successful when the inspection shows that the payload materials are either nonflammable or self-extinguishing per NHB 8060.1, or that sufficient justification has been approved for their use.

A flammability assessment has been performed and is listed / rationalized in the MIUL. Wherever possible, A-rated materials have been used. A few selected materials are B- or U-rated. Their use has been rationalized, and they were approved for flight on STS-77, STS-83 and STS-94, by independent review through McDonnell Douglas and Teledyne Brown. The flammability assessment was reviewed for STS-77 by McDonnell Douglas (now Boeing Spacehab) in Huntsville, and for STS-83 / STS-94 by Teledyne Brown Engineering, David Ezell.

The updated MIUL has been compared to the as-built hardware for STS-112. The hardware has been inspected for the proper rationale used in the MIUL for flammability assessment and rationale for use of material.

7. Verification of toxic offgassing by payload hardware shall be by test. A test shall be conducted on all payload hardware per the conditions and criteria of NASA-STD-6001, Test 7, to determine the suitability of the payload nonmetallic materials and assembled articles used in crew compartment environments with respect to toxic offgassed products. The verification shall be considered successful when the test results show the payloads in habitable areas meet the toxic offgassing acceptance criteria of NASA-STD-6001, Test 7.

The PGBA payload assembly has been offgas tested at MSFC per NASA-STD-6001, test 7 / NHB8060.1C, for mission STS-77. The tests were performed in conjunction with the FGBA payload. Tests data (see attachment 1) therefore contains offgas data for BOTH payloads (FGBA and PGBA). Since then, many years have passed. Since both PGBA and FGBA were new at time of test, and offgassing from new foams, cleaning solvents, adhesives, have since ‘aged’, the actual PGBA offgas data by time of flight STS-112 will be MUCH LESS than those values given in Attachment 1. Some components were replaced with ‘like-items’ for STS-112 (such as new labels, connectors). As they replace items of same material, no impact on offgas data. The PGBA payload passed the test, with a SUMT100 of 0.064221125, with a max. unit limit of 7.7 units (A-rated). Please note that this rating is for PGBA and FGBA, we only fly PGBA. Given the similarity of PGBA and FGBA, sound engineering judgment would indicate that the actual PGBA values are approximately ½ of those listed in Attachment 1.

8. Verification of dissimilar metals compatibility shall be by inspection or analysis. The inspection shall compare the materials and parts list with the materials listed in MSFC-SPEC-250, Table III. Verification shall be considered successful when the inspection of the materials and parts list shows that the internal materials used in the integrated rack aqueous fluid systems are compatible according to the table specified. Analysis shall be performed on materials not listed in MSFC-SPEC-250, Table III. Verification shall be considered successful when the analysis of the materials shows that the internal materials used in the integrated rack aqueous fluid systems do not create a dissimilar metal couple greater than 0.25 V with the ISS aqueous fluid system.

Not applicable, as PGBA does not use the ISS fluid system.


9. Verify by inspection that payloads which are intended to remain on-orbit for more than 1 year uses materials that are non-nutrient per the requirements of SSP 30233, par 4.2.10. If a fungus-nutrient material must be used, verify by inspection that it is treated to prevent fungus growth, or that its usage satisfies the requirement. Inspection of design drawings and materials lists shall determine whether fungus-resistant materials have been used as required. Verification shall be considered successful when the inspection shows fungus-resistant materials are used as required.

Not applicable, as PGBA-04 does not use the fluid system.

Summary of analysis and test reports

Planned Releases All operational modes of PGBA have been reviewed and at no time during its continuous operations in both the orbiter middeck and in the EXPRESS Rack will there be any planned release of materials, with exception of respiratory gas exchanges of plants with cabin air, at cabin air concentrations, at peak exchange rates of 0.01 to 0.001 times those of one human being.

Nominal Releases PGBA will of course evolve gasses over its lifetime, just as any other payload, with non-metallic materials. The offgas characteristics of PGBA were determined via a Toxic Offgassing test run, with test results printed on February 29, 1996 (See attachment 1, MSFC). The payload was subject to the NHB8060.1C test 7 procedures, with a max. unit limit of 7.7 See attached MSFC test report in Attachment 1. These data are still valid for STS-112. Pre-launch cleaning of flight hardware will be accomplished using a citrus-based solvent or similarly approved cleanser, as provided by Hangar-L or SSPF.

Determination PGBA nominal/planned release of materials falls within acceptable parameters.

Materials Compatibility All materials compatibility issues have been reviewed and incorporated into the PGBA payload hazard reports. These have been previously signed by the PSRP for STS-77 (baseline) and will be re-baselined without changes for new documentation references at the PGBA Phase 3 reflight review on January 23/24, 2002.

The hazard reports verify: 1. All levels of containment within PGBA (plants, water, nutrient solution, chemicals such

as Barium Hydroxide, Activated Charcoal, Potassium Permanganate, Titanium Dioxide catalyst, coolants fluid).

2. All fluids contained and approved per the HMST (Hazardous Materials Summary Table – V1 Letter).

3. Only approved fluids loaded at quantities and qualities less than or equal to those listed in the HMST (JSC Toxicology V-2 letter at L-1 Day Handover).

4. Compatibility tested for 1.5 times the nominal mission duration, to account for potential delays in the payload’s return.

Those hazard reports are: 1. STD-PGBA Offgas test, mercury, battery electrolyte, flammability. 2. PGBA-7 Containment of fluid samples (excl. coolant fluid).


3. PGBA-11 Batteries (battery electrolyte). 4. PGBA-13 Pressurized System – PGBA Coolant System.

Determination: PGBA is capable of safely containing all materials. All controlling hazard reports, analyses, the SVTL, and the HMST are on file and can be requested if necessary. All materials have been previously approved, and offgas test results are attached.

PGBA4 Submittal MP-ER-001 – item 3: The MIUL and all associated documents (offgas, flammability assessment, stress corrosion assessment) have been provided to MSFC / EXPRESS for review. We are awaiting concurrence from the MSFC / EXPRESS assigned independent review of our submittals. Once obtained, we will forward a letter of approval / concurrence, and the MUA once issued.

01 December 2001

Alex Hoehn, Ph.D. Associate Director Engineering - BioServe Space Technologies Assistant Research Professor - Aerospace Engineering Sciences Campus Box 429 - Boulder CO 80309-0429, USA +1-303-492-5875 phone / +1-303-492-8883 fax email: mailto:[email protected] web: http://spot.colorado.edu/~hoehn/ http://www.colorado.edu/engineering/BioServe/ http://www.colorado.edu/ASEN/IMS/


Attachment 1 – Offgas Data



Attachment 2 – Environmental Compatibility The PGBA-04 payload will be cleaned prior to shipment to KSC, and will be re-cleaned prior to handover. At that point, a certificate of cleanliness will be signed and provided at handover. All surfaces are cleaned using approved cleaning agents, provided by Hangar-L or SSPF (typical citrus cleaner, and historically isopropyl alcohol). “KSC ISS-Ut ilization” personnel (a.k.a. Jeannie Ruiz and colleagues) ALWAYS re-clean, and re-verify cleanliness at handover, prior to moving the payload to the launch pad. All PGBA accessible exterior and internal surfaces are compatible with the listed and approved cleaning agents. The materials compatibility analysis is on file. Most surfaces are metal (anodized aluminum or steel), with some polycarbonate surfaces (light box, plant chamber box, LCD screen frame, LED lenses and lens covers / holders), and Teflon-insulated wire harnesses. These non-metallic surfaces are all compatible with the approved and customary solvents. See attachment 1 – Materials Compatibility Analysis for materials exposed to cleaning agents or chemicals in potential contact during laboratory work at Hangar L, SSPF or during payload integration at the pad.

LCD Screen: Test item Test condition Evaluation standard Storage at high humidity 65 C 90%RH 240 hours R/Ro < 1.6 Storage at high temp. 80°C 240 hours R/Ro <1.2 Storage at low temp. -30°C 240 hours R/Ro < 1.2 Heat shock -30°C 1 hr <--> 80°C 1 hr (10 cycles) R/Ro < 1.2 Anti-static electricity Discharge the touch screen center and its

surrounding 20 times R/Ro < 1.2

Insulation resistance DC100V and 100M ohm or more Pass test with good results Withstand voltage DC125V for 1 min. or less Pass test with good results Wear resistance Steel wool 10mm x 300mm 300g 10 times No visual scratch Note: R=Resistance after test, Ro=Initial resistance Touch Screen Chemical Resistance 5% NaOH 5 hr immersion 28% NH4OH 12 hr immersion 35% HCL 0.5 hr immersion Toluene 24 hr immersion Acetone 24 hr immersion Methyl ethylketone 24 hr immersion Ethyl acetate 24 hr immersion Butyl acetate 24 hr immersion Ethanol 24 hr immersion

No degradation of touch screen appearance was present

Materials Compatibility of Exposed PGBA Components Chemical Polycarbonate Acetone D- Severe Effect Alcohols:Amyl B1- Good Alcohols:Benzyl N/A Alcohols:Butyl A2- Excellent Alcohols:Diacetone N/A Alcohols:Ethyl B2- Good Alcohols:Hexyl N/A Alcohols:Isobutyl N/A Alcohols:Isopropyl A2- Excellent Alcohols:Methyl B1- Good Alcohols:Octyl N/A Alcohols:Propyl N/A Detergents A1- Excellent Diacetone Alcohol D- Severe Effect


Dichlorobenzene D- Severe Effect Dichloroethane D- Severe Effect Diesel Fuel A2- Excellent Diethyl Ether D- Severe Effect Diethylamine D- Severe Effect Diethylene Glycol B1- Good Ethanol B2- Good Gasoline (high-aromatic) A- Excellent Gasoline, leaded, ref. A2- Excellent Gasoline, unleaded A2- Excellent Isopropyl Acetate D- Severe Effect Isopropyl Ether D- Severe Effect Isotane N/A Jet Fuel (JP3, JP4, JP5) A1- Excellent Kerosene D- Severe Effect Ketones D Severe Effect Lacquer Thinners B Good Lacquers D Severe Effect Lithium Hydroxide D- Severe Effect Lye: Ca(OH)2 Calcium Hydroxide D- Severe Effect Lye: KOH Potassium Hydroxide D- Severe Effect Lye: NaOH Sodium Hydroxide D- Severe Effect Methyl Ethyl Ketone (MEK) D- Severe Effect Methylene Chloride D- Severe Effect Mineral Spirits C- Fair Oils:Citric A- Excellent Oils:Fuel (1, 2, 3, 5A, 5B, 6) B- Good Oils:Mineral B- Good Oils:Olive A2- Excellent Oils:Orange C1- Fair Oils:Pine A- Excellent Potassium Permanganate A2- Excellent Propylene Glycol B1- Good Salicylic Acid A1- Excellent Salt Brine (NaCl saturated) A- Excellent Sea Water A2- Excellent Silicone A2- Excellent Silver Bromide N/A Silver Nitrate A2- Excellent Soap Solutions A1- Excellent Soda Ash (see Sodium Carbonate) A- Excellent Sodium Acetate A1- Excellent Sodium Hydroxide (20%) A2- Excellent Sodium Hydroxide (50%) D- Severe Effect Sodium Hydroxide (80%) D- Severe Effect Vinegar A2- Excellent Vinyl Acetate N/A Vinyl Chloride N/A Water, Acid, Mine B2- Good Water, Deionized N/A Water, Distilled A2- Excellent Water, Fresh A2- Excellent Water, Salt A2- Excellent Weed Killers N/A Whey N/A Whiskey & Wines A1- Excellent Xylene D- Severe Effect


Attachment 3 – Materials Usage Summary for STS-112 / ISS.9A. PGBA-04, the configuration flying on STS-112, has been updated to new ISS requirements. The majority of the PGBA components are unchanged from previous flights on STS-77, STS-83 and STS-94. The changes are minor, and do not invalidate offgas, flammability or stress corrosion assessments and approvals from previous missions.

Changed Item Description Electric Connector Change-out

The main power and data connectors were replaced with like units that meet the new EXPRESS pin assignments. Connectors use steel chassis with Silicon rubber inserts. New connectors air same manufacturer / same materials as old ones, only new pin assignments and different geometry. Program provided. All A-rated materials.

Labels After three successful flights and no problems with on-orbit flight operations, Human Factors engineer required label changes to enhance the usability of the payload. Existing labels were replaced with labels of same material and size, but with greatly enhanced choice of words, which will make the autonomous operation of PGBA even more successful. No new materials.

Circuit Breakers Four of the 5 existing circuit breakers were removed to streamline the PGAB operations. This removed non-metallic materials. No new materials, actually less materials than before.

Muffler Addition Designed by Boeing as Government Furnished Equipment (GFE) from A-rated materials only. Fully enclosed 6061 T6 aluminum box with foam core for sound suppression. No electric wiring, only airflow passageway. Johnson Engineering under contract to Boeing certified all materials as A-rated. No issues. Same design flown on STS-100 and STS-110 for CGBA. The GFE mufflers are attached with Velcro to the payload. The Velcro strips are all << 4” in length and widely separated from each other. The GFE-supplied flammable white Nylon Velcro was replaced with flame -retardant beige Velcro.

Captive Fasteners The original PGBA mounting used non-captive GFE fasteners for the interface between PGBA and the Payload Mounti9ng Panel. The new requirement requires captive fasteners provided by the PD to allow on-orbit removal of PMPs. The fasteners were selected from EXPRESS-recommended fasteners, manufactured from certified materials from approved vendors. They are fracture critical, and are uniquely tracked by other PVP requirements. They are metallic, from MSFC-A-rated materials with re4spect to stress corrosion.

Nomex Covers The 0.5” Pyrell foam used within PGBA as a vibration isolation foam was originally uncovered and contained within the PGAB double locker shell. Since flight crew now gains access to the PGAB interior space, the exposed Pyrell foam was covered with Nomex for beautification. This reduces greatly the risk of flaking / tears in the Pyrell foam. It has no impact on the flammability assessment, as the entire shell acts as a flame barrier with respect to the vibration isolation foam. It only reduces wear and tear on the foam. Same Nomex used by Spacehab and on all CGBA units for the CGBA ‘sleeping bag’ payload wrap.

Video cameras The existing 1995 video cameras were replaced with a smaller, updated video camera assembly of newer date (2000). These cameras are single board miniature high-resolution cameras. The new cameras are actually only ¼ of the size, thereby greatly reducing the amounts of non-metallic materials such as circuit board assemblies. Commercial of the Shelf Units, same materials as before, just fewer amounts.

Brass Fittings All non-stressed brass fittings listed in the earlier PGBA MIUL were replaced with Stainless Steel fittings. The original brass fittings were used in the PGBA atmosphere treatment system. The rated pressures of 600 to 3000 psi, versus the actual dead head pressure of the miniature compressor of 14 psi led to the approval of these brass fittings on previous flights. To avoid further discussions and additional cost and continued re-justifications of the use of brass fittings, the fittings were replaced with their stainless steel replacement units. The MIUL was updated. The parts are tracked in hazard report PGBA-13 (pressurized system).

Liquid Coolant System The original PGBA unit used a single water pump to drive a split coolant system. This


resulted in performance limitations. With the implementation of the new CGAB water circulation pump on STS-106, this pump design is now also implemented into PGBA. The pump assembly is only ¼ of the size of the old PGAB pump design (Same manufacturer, same design), but two pumps are used to drive each coolant system with its own pump. The net total is fewer components. The new pump is also used on all CGBA payloads, and features stainless steel pump heads, and a brush-less DC motor. The DC motor driving the new pump head is actually the same motor as the old PGBA pump; therefore no new non-metallic materials were added.

Plant Chamber Lid Closure

The plant growth chamber lid was originally attached with 28 individual non-captive cap screws. Since the flight crew gains access to the chamber for plant harvesting, the stainless steel non-captive screws were replaced with stainless steel captive screws. No new non-metallic materials.

Computer Disk The previous Solid State Disk (SSD) of PGBA was only 40 MB big (Sandisk). The new Sandisk Solid State Disk holds 300 MB, and is less than 1/6 in size. It is a commercial off the shelf Sandisk. Same type of solid-state memory assembly, but much fewer components and much smaller. Same as CGBA payload or any digital camera (Compact Flash). Less material than before.

Summary The materials changes have resulted in fewer non-metallic components, and fewer stress-corrosion prone materials. As such, all changes have enhanced the safety of the payload, and removed questionable items criticized by previous reviews through McDonnell Douglas and Teledyne Brown Engineering. Sound engineering judgment seems to indicate that this is good.

Figure 1. The PGBA-04 configuration for STS-112 / ISS.9A, showing the added mufflers (right), the flame-retardant Nomex (left, for muffler attachment), and the new connectors / removed circuit breakers. The new labels use same materials, but greatly enhanced choice of words to improve the safety and usability of the payload at the request of Human factors. The IMS label is GFE equipment, and nothing is known about its flammability and offgas characteristics, as it is program-provided. Since the NASA-provided fire hole sticker is X-rated for flammability, we assume that the new IMS labels are also highly flammable.


Attachment 4 – Materials Usage Summary by Teledyne Brown Engineering for STS-83 (David Ezell).

PGBA General Description The Astro-PGBA is a facility to support the growth of plants in a microgravity environment. The Astro-PGBA is developed by a consortium of interest led by BioServe Space Technologies, a NASA Commercial Space Center located at the University of Colorado. Astro-PGBA supports plant growth by providing light, atmosphere control (gas composition, temperature, humidity), nutrient delivery, and data acquisition (including video and plant performance data). Astro-PGBA was flown on the Spacehab 4 mission (STS-77) prior to MSL-1.

Figure 2. The PGBA uses a double-middeck locker sized aluminum enclosure module (locker replacement). External heat rejection is accomplished through forced convective cooling to cabin air. All control interfaces are on the front panel. The payload will be opened on ISS for access to the plant chamber, plant harvesting and re-seeding. The hinged faceplate can be rotated into the open position by opening the 4 NSTS locker latches.

Astro-PGBA occupies two standard middeck locker spaces, and will be mounted in the orbiter middeck for ascent and descent. Following on-orbit activation of the EXPRESS Rack, tow of the storage lockers will be removed from the EXPRESS and transferred to the Orbiter middeck. Astro-PGBA will be removed from the Orbiter middeck, installed in the space acquired by the removal of the middeck lockers, and interfaces with EXPRESS-provided power and signal interfaces. Astro-PGBA will be returned to the Orbiter middeck prior to module closeout. The unit is a reflight from Spacehab-4 mission with the exception that a Barium Hydroxide canister was redesigned for mass savings. Barium Hydroxide is used for carbon dioxide removal, which is produced by the plants during the night cycles. JSC safety has approved the use of all filter systems to keep a controlled atmosphere in the plant growth chamber.


Figure 3. Transfer of PGBA from middeck to Spacelab EXPRESS on MSL-1 (STS-94).

Figure 4. PGBA-03 operated inside proto-EXPRESS, STS-94, in middeck configuration without mufflers (left), and in ISS configuration with mufflers (right). These pictures show the STS-94 configuration with 5 circuit breakers / LEDs and the old NSTS connectors. For STS-112, 4 of the 5 circuit breakers /LEDs were removed, and the NSTS connectors were replaced with program-provided ISS EXPRESS connectors.

Stress Corrosion Cracking Assessment The Materials Identification and Usage List (MIUL) identified several Table III alloys per MSFC-SPEC-522 that were utilized in the design of the Astro-PGBA. The PGBA unit is mounted in the middeck in a double-locker replacement unit during ascent and descent, and is transferred to the EXPRESS rack for on- orbit operations. The double-locker and the PGAB containment structure are all built from A-rated and certified materials. There are no major structural items that, if they failed, would cause a safety hazard. Below is a brief description of those alloys that were identified as being less than highly resistant to stress corrosion and acceptance rationale. • Aluminum 2023-T3 honeycomb structure used as a base plate for the internal structure. This is an error in the

MIUL; the actual material used was Al6061-T6, an acceptable material. • Aluminum 2024-T3 corners and face sheets in the plant chamber. The face sheets are internal false wall

deflector sheets, separating the upstream and downstream internal air circulation. They are not under a sustained tensile load. The corner brackets are not loaded; they are used only to "square up" the chamber. No tensile load to induce stress corrosion and these parts are non-structural.

• Thermal Control/Water system utilizes several unidentified alloys in the pump system. This pump is used to provide water to the plants. No safety hazard to the crew or other hardware exists if this water system should fail.

• Atmosphere Control System uses brass parts in a non-structural application. System is used to circulate air through plant growth chamber. No safety hazards if parts should fail.


Toxicity Assessment The Astro-PGBA unit was offgas tested prior to flight aboard the STS-77 mission, which was the Spacehab-04 mission. The unit passed with a T value of 0.064221 when tested with the FGBA, and the results were reported in memorandum EH42B(96-0047), which is attached.

Flammability Assessment The Astro-PGBA is a self-contained plant growth chamber. It was necessary in the design of this chamber to utilize some non-metallic materials that either are flammable, or no flammability data exists in the NASA materials database. These materials and acceptance rationale is listed below.

Shell Assembly (Double-Locker) Double sided 950 Scotch tape (no data) is used to adhere uncoated Pyrell foam (material code 05733, rated "x" for flammability) to the aluminum sides of the shell assembly to isolate the internal payload components from the shell. When the outer containment shell is installed, the Pyrell is sandwiched between metal with no ignition sources. No particles that are unintentionally generated by the Pyrell can escape after the outer containment shell is installed.

Structure Faceplate The connector backshells are all metallic. The circuit breakers and switches are a Mil-Spec plastic with metal contacts. There are LEDs at the front of the faceplate that are covered with a polycarbonate lens and are spaced one inch apart.

Plant Chamber Structure An adhesive Masterbond EP21LV is used to bond metal-to-metal surfaces together in the honeycomb structure. Obviously this adhesive is sandwiched between metal surfaces. Lexan 9034 is used in the chamber, but is not near any ignition sources.

Root Tray Assembly Small tray in which the plants are potted. Primarily Lexan 9034, but no ignition sources. Norprene (material code 89838 “X” -rated for flammability) is used to transport water into tray, no ignition sources. Norprene is a polypropylene and offers excellent flexibility, low offgassing and biocompatibility.

Air Plenum and Blower The blower fan is made from a material Ultramid A3XG5, which is polyamide with 50% fiberglass. No ignition sources. This is a commercial fan assembly with UL, CSA, VDE approvals.

Plant Chamber Electronics The plant chamber is enclosed in a metallic housing. All electronics components are enclosed in this housing.

Humidity Control System The humidity control system is enclosed in a metallic housing. Norprene tubing is used to transport water, all wiring is Teflon insulated. A polyethylene reservoir stores water for use within the plant chamber.

Temperature Control Electronics Sensors are embedded in aluminum structures (heat exchangers). All switches solid-state relays. All items are heat sunk.

Carbon Dioxide Removal System BaOH is contained in a protected aluminum cartridge. The BAOH has a 40 µ filter. If it leaked, the BaOH would go to the plant growth chamber, which is a totally contained unit. A hydrophobic Millipore filter allows air to pass.


Ethylene Removal System Photocatalytic unit contains UV-lamps. Enclosed in a polycarbonate body. No containment except for outer shell. This is the 4th flight of this system (Astroculture, WCSAR).

Water Containment System The plant chamber uses a hydrophobic Millipore polypropylene filter to allow air to pass, but to contain potential water within the plant growth chamber. No ignition sources.

Atmosphere Control System, Norprene tubing utilized in system to transport water. No ignition sources.

Atmosphere Control Electron9ics All wiring is Teflon insulated. Contained in metallic housing.

Nutrient delivery System Polypropylene nutrient packs supplied by NASA Ames. Commercial micropumps remote from ignition source.

Video System Miniature cameras installed inside metallic sealed light box.

Light Box Assembly Considered a sealed metallic container. No propagation paths. All wiring is Teflon insulated. Mercury vapor lights are commercial GE compact fluorescent lamps. Containment approved by JSC PSRP.

Computer Assembly Enclosed in Aluminum 6061T6. No propagation paths.

Power Assembly Mounted to metal faceplate, DCDC converters are in a metal housing.

Wire Harness All wiring is Teflon insulated (200°C). All connectors are potted with either RTV 3140 or RTC 3145.


PGBA Picture

Figure 5. PGBA-04 opened, showing the internal plant growth chamber (aluminum honeycomb / epoxy) with polycarbonate lid, the light box (aluminum enclosure with polycarbonate lid), and the aluminum heat exchanger assemblies with thermoelectric coolers. The nutrient delivery system and the plants are contained in the polycarbonate root tray assembly within the plant growth chamber.

Figure 6. PGBA-04 Inner Guts - Side views: Left side has atmosphere treatment system, solid state AC inverter ballasts for lamps, and one of the two water heat exchangers. Right side has computer assembly, solid-state relays and the second of two water heat exchanger assemblies. All wire harnesses use twisted pair, or twisted pair shielded wire, with 200°C Teflon insulation.


Figure 7. PGBA-04 Inner Guts. Left: – Back View. Computer assembly in left corner, atmosphere treatment system in right corner. Plant chamber above Right: Plant Chamber can rotate open (clam shell) to gain access to plants. Computer assembly below plant chamber on right side.

Figure 8. PGBA-04 Back of Faceplate. Left: Light box contains fluorescent lamps and video cameras in intentionally vented container. Heat exchanger assembly is mounted to the plant growth chamber, and discharges cabin air into the PGBA “avionics bay” between the light box and the faceplate. The solid-state inverter ballast (3 metal boxes on right) and the solid state relay switches (left next to wire harness) are all within the fan-driven cabin air coolant flow. The PGBA power system is mounted behind the light box onto the PGBA faceplate, and is cooled by the coolant airflow.


Attachment 5 – Materials Usage Summary by McDonnell Douglas for STS-77.





-----Original Message----- From: Beatty, Glen [mailto:[email protected]] Sent: Friday, October 20, 2000 3:57 PM To: 'Hoehn, Alex' Cc: Koelle, William A Subject: STS-95 Verification Alex, As you know, the Boeing Huntsville SPACEHAB program was responsible for the integration efforts of all SPACEHAB module and middeck payloads for the STS-95 mission. As you also know, CGBA was one of the payloads on the STS-95 mission manifest. All verification requirements for all payloads, including CGBA, that flew on the STS-95 mission were closed prior to the launch of that mission. These verification requirements had as a source, ICD based interface requirements and safety requirements, which were based on the payload form 1230s and unique Payload Hazard Reports. Most STS-95 payloads, including CGBA, had safety verification requirements that were associated with materials. Again, all of STS-95 verification requirements, including those safety based CGBA requirements associated with materials (including toxicity, flammability, stress corrosion cracking, hazardous sample containment, etc.) were closed by the standard Boeing verification process. With regard specifically to the MIUL submitted by BIOSERVE to address the flammability hazard control, the Boeing assessment of this MIUL, which is documented in Boeing document MDC 98W5732, the "STS-95 Verification Assessment Report", dated October 1998, is as follows: "An MIUL has been submitted for the GEFA, BPCS and computer assembly. All non-metallic materials were shown to be "A" rated or appropriate rationale was provided. A note of additional info.: The MIUL for the GEFA included one item (PTFE Membrane) for which the flammability rating is shown as "U"; this material, in nearly the same thickness, has been tested and included in MAPTIS as Material Code 60162." Based on this assessment, we determined that the MIUL was sufficient for closing the associated hazard control. Glen Beatty Manager - SPACEHAB Mission Support Engineering The Boeing Company P.S. Alex, it seems the tables are turned, and I am now providing you a Certificate of Conformance!! I hope this fulfills your needs. If not, feel free to call me at home this weekend at 256-539-5586, or page me at 1-800-946-4646, PIN 145-4498. I'm outta here.

PGBA4 - MIUL - TOTAL MASS - STS112/ ISS.9A 16-Jan-02

MASS IN GRAMSUBSYSTEM SUBASS SUBASSC

STRUCTURE SHELL ASSEMBLY 11585.20PG110-00 GRAMSTR SA

FACE PLATE ASSEMBLY 2352.75PG120-00 GRAMFP

INTERNAL STRUCTURE 1351.10PG130-00 GRAMINS

SILENCER KIT / MUFFLER 3940.50PG140-00 GRAMMUF

PLANT GROWTH CHAMBER PLANT CHAMBER STRUCTURE (210/260) 3707.30PG210-00 GRAMpgc pcs

ROOT TRAY ASSEMBLY 291.93PG212-00 GRAMRTA

AIR PLENUM, BLOWER 2052.63PG213-00 GRAMAPB

PLANT CHAMBER ELECTRONICS 271.97PG214-00 GRAMPLE

THERMAL ASSEMBLIES TEMPERATURE CONTROL SYSTEM 1328.00PG221-00 GRAMTH TCS

HUMIDITY CONTROL SYSTEM 1538.30PG222-00 GRAMHCS

TEMPERATURE CONTROL ELECTONICS 368.64PG223-00 GRAMTCE

THERMAL CONTROL, AIR 2578.00PG224-00 GRAMTCA

ATMOSPHERE COMPOSITION ASSEMBLY CARBON DIOXIDE SYSTEM 389.60PG231-00 GRAMATS CDS

ETHYLENE REMOVAL SYSTEM 258.40PG232-00 GRAMERS

ACTIVATED CARBON SYSTEM 389.60PG233-00 GRAMACS

WATER CONTAINMENT SYSTEM 240.80PG234-00 GRAMWC

ATMOSPHERE CONTROL 904.10PG235-00 GRAMATC

ATMOSPHERE ASSEMBLY ELECTRONICS 925.90PG236-00 GRAMAAE

NUTRIENT DELIVERY ASSEMBLY NUTRIENT PACKS 4650.00PG241-00 GRAMNDA NP

NUTRIENT DELIVERY SYSTEM 122.60PG242-00 GRAMNDS

NDS2 - AUTOMATIC GERMINATION 1167.09PG245-00 GRAMNDS

LIGHTING SYSTEM VIDEO SYSTEM 278.00PG251-00 GRAMLT VS

LIGHT BOX STRUCTURE 1394.02PG252-00 GRAMLBS

LIGHTING SYSTEM ELECTRONICS 1366.40PG254-00 GRAMLSE

ELECTRIC ASSEMBLIES COMPUTER ASSEMBLY 1467.97PG310-00 GRAMEL CA

LCD ASSEMBLY 750.50PG320-00 GRAMLA

POWER ASSEMBLY 838.60PG330-00 GRAMPA

WIRE HARNESSES 2364.20PG340-00 GRAMWH

ELECTRICAL MISCELLANEOUS 800.80PG350-00 GRAMEMS

49674.89GRAND TOTAL (metric):

109.28

GRAM

LBM.GRAND TOTAL (imperial):

PGBA PLANT GENERIC BIOPROCESSING APPARATUS MIUL / Parts List Page 1 of 61

Page 1 of 61

SUB SUBCAT ASSEMBLY SUBASS SUBASSCAT SUBASSNSTR STRUCTURE PG100-00 SA SHELL ASSEMBLY PG110-00

FP FACE PLATE PG120-00INS INTERNAL STRUCTURE PG130-00MUF SILENCER KIT / MUFFLER PG140-00

PG260-00 PCS PLANT CHAMBER STRUCTURE PG260-00

PGC PLANT GROWTH CHAMBER PG210-00 RTA ROOT TRAY ASSEMBLY PG212-00APB AIR PLENUM AND BLOWER PG213-00PLE PLANT CHAMBER ELECTRONICS PG214-00

TH TEMPERATURE CONTROL PG220-00 TCS THERMAL CONTROL SYSTEM PG221-00HCS HUMIDITY CONTROL SYSTEM PG222-00TCE TEMPERATURE CONTROL ELECTRONICS PG223-00TCA THERMAL CONTROL, AIR PG224-00

ATS ATMOSPHERE COMPOSITION ASSEMBLY PG230-00 CDS CARBON DIOXIDE SYSTEM PG231-00ERS ETHYLENE REMOVAL SYSTEM PG232-00ACS ACTIVATED CARBON SYSTEM PG233-00WCS WATER CONTAINMENT SYSTEM PG234-00ATC ATMOSPHERE CONTROL PG235-00AAE ATMOSPHERE ASSEMBLY ELECTONICS PG236-00

NDA NUTRIENT DELIVERY ASSEMBLY PG240-00 NP NUTRIENT PACKS PG241-00NDS NUTRIENT DELIVERY SYSTEM PG242-00NDE NUTRIENT DELIVERY ELECTRONICS PG243-00

LT LIGHTING SYSTEM PG250-00 VS VIDEO SYSTEM PG251-00LBS LIGHT BOX STRUCTURE PG252-00LC LIGHTING COMPONENTS PG253-00LSE LIGHTING SYSTEM ELECTRONICS PG254-00

EL DACC/ELECTRIC PG300-00 CA COMPUTER ASSEMBLY PG310-00LA LCD ASSEMBLY PG320-00PA POWER ASSEMBLY PG330-00WH WIRE HARNESS PG340-00EMS ELECTRICAL MISCELLANEOUS PG350-00SEN SENSOR ASSEMBLY PG360-00

TOXICITY RATINGS ARE NOW BASED ON MAXIMUM LIMIT WEIGHT (ML WGT) CALCULATED FROM SUMMATION OF T EQUAL TO .5 -- RATINGS SHOW USE WEIGHT OF MATERIAL AFTER ALL CURES, IF APPLICABLE, ARE MET. B DATA INCONCLUSIVE -- BATCH VARIATIONS. WORST CASE CURE IS GIVEN. MATERIAL SHOULD BE TESTED PRIOR TO USE. TOXICITY RATINGS MEET REQUIREMENTS IN NASA-STD-6001.NOTE: MATERIALS PREVIOUSLY RATED "B" INDICATED A SPECIAL CURE.

K MAXIMUM LIMIT WEIGHT >= 100 LB (45400 GRAMS)H MAXIMUM LIMIT WEIGHT >= 50 LB (22700 G) < 100 LB (45400 G)A MAXIMUM LIMIT WEIGHT >= 10 LB ( 4540 G) < 50 LB (22700 G)V MAXIMUM LIMIT WEIGHT >= 5 LB ( 2270 G) < 10 LB ( 4540 G)X MAXIMUM LIMIT WEIGHT < 5 LB ( 2270 G)I MATERIALS WITH INSUFFICIENT DATA.

A ASSEMBLED ARTICLES WHERE T VALUE IS .5 OR LESSX ASSEMBLED ARTICLES WHERE T VALUE IS GREATER THAN .5

A MATERIALS ARE RATED "A" IF THEY MEET THE REQUIREMENTS OF MSFC-SPEC-250A, CLASS II, AND DO NOT REQUIRE A COATING.

B MATERIALS ARE RATED "B" IF THEY MEET THE REQUIREMENTS OF MSFC-SPEC-250A IF COATED.

X MATERIALS FAILS REQUIREMENTS.

A MATERIALS WITH SAMPLE MEASUREMENTS/TEST CONDITIONS RECOMMENDED IN NASA-STD-6001 BURN LENGTH OF 6 in. (15cm) OR LESS, NO DRIP BURNING OR SMALL DRIP BURNING AND NO IGNITION OF K10 PAPER. STANDARD TEST IS 3 SAMPLES.(CAN FAIL BUT NOT PASS ON LESS THAN 3) CONFIGURATION TEST CAN BE RATED ON ONE, TWO OR THREE SAMPLES.

B MATERIALS THAT HAVE A BURN LENGTH OF MORE THAN 6 in. (15cm) BUT LESS THAN 12 in. (30cm) IN TEST 1, NO DRIP BURN OR SMALL DRIP BURN AND NO IGNITION OF K10 PAPER. STANDARD TEST IS 3 SAMPLES.(CAN FAIL BUT NOT PASS ON LESS THAN 3) CONFIGURATION TEST CAN BE RATED ON ONE, TWO OR THREE SAMPLES.

C MATERIALS THAT BURN TOTALLY WITH NO DRIP BURN OR SMALL DRIP BURN WITH NO IGNITION OF K10 PAPER. X MATERIALS IGNITE K10 PAPER WITH SMALL, MODERATE OR LARGE DRIP BURNING. THE BURN LENGTH IS NOT A FACTOR. S SPECIAL TEST CONDUCTED ON MATERIALS. I LESS THAN 3 STANDARD SAMPLES WITH LESS THAN 12 in. (30cm) BURN. NO BURN DRIP OR NO IGNITION OF K10 WITH SMALL DRIP BURNS.

A MATERIALS ARE RATED "A" IF THEY ARE LISTED IN TABLE 1 OF MSFC-SPEC-522A AS HAVING HIGH RESISTANCE TO STRESS CORROSION.

B MATERIALS LISTED IN TABLE 2 OF MSFC-SPEC-522A.

C MATERIALS LISTED IN TABLE 3 OF MSFC-SPEC-522A. N MATERIALS ARE RATED "N" IF NOT APPLICABLE TO STRESS CORROSION CRACKING OR NOT USUALLY USED IN DESIGN.

Page 2 of 61PGBA MATERIALS RATING per MSFC

STRESS CORROSION CRACKING SUSCEPTIBILITY TEST RATING CORROSION RESISTANCE TEST RATING

FLAMMABILITY (TEST 1, TEST 10) RATINGTOXICITY / OFFGAS

PGBA PLANT GENERIC BIOPROCESSING APPARATUS

MIUL MATERIAL IDENTIFICATION AND USAGE LIST

SUBSYSTEM: STRUCTURE

SUBASSEMBLY: SHELL ASSEMBLYASSEMBLY DRAWING: PG110-00

M/N DESCRIPTION QTY PART NO.DWG. NO.

MANUFACTURERSUPPLIER

MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]

F T C S REMARKS / Usage Rationale / Missions Flown (A=all, 1=STS77, 2=STS83, 3=STS-94, 4=STS112

STS-112 PGBA-04 Page 3 of 61

STR

SA

M CAPTIVE FASTENER, SLEEVE BOLT 8 FIT A286, CRES300 125.60 A A NEW FOR STS112: SILVER PLATED FOR PMP / EXPRESS I/F

CS5001-4-7 4

M CAPTIVE FASTENER, RETAINER NUT

8 FIT A286, CRES300 16.00 A A NEW FOR STS112CSR523-4-2 4

M RIVET, 1/8" DIA X 5/16" L, UNIV. HEAD

160 HANSON RIVET AL 7075.T73 1,418.00 B A CHROMATEMS20426-AD4-5 A

M RIVET, 1/4" DIA X 3/4" L, 100 CSK. HEAD

72 HANSON RIVET AL 7075.T73 B A CHROMATEMS20426-B8-12 A

M DOUBLE LOCKER, PAYLOAD MOUNTING BRACKET

4 BST AL 7075.T7351 1,052.40 B A ANODIZED MIL-A-8625, TYPE II, CLASS 1 / CHROMATE, MIL-C-5541

PG110-01 A

M DOUBLE LOCKER, FRONT MOUNTING BRACKET

4 BST AL 7075.T7351 548.00 B A ANODIZED MIL-A-8625, TYPE II, CLASS 1 / CHROMATE, MIL-C-5541

PG110-02 A

M DOUBLE LOCKER MOUNTING RING 1 BST AL 6061.T651 311.60 B A ANODIZED MIL-A-8625, TYPE II, CLASS 1 / CHROMATE, MIL-C-5541

PG110-03 A

M DOUBLE LOCKER CORNER BRACKET

4 BST AL 6061.T651 1,204.80 B A ANODIZED MIL-A-8625, TYPE II, CLASS 1 / CHROMATE, MIL-C-5541

PG110-04 A

M DOUBLE LOCKER SIDE PANEL 2 BST AL 6061.T651 3,518.00 B A ANODIZED MIL-A-8625, TYPE II, CLASS 1 / CHROMATE, MIL-C-5541

PG110-05 A

M DOUBLE LOCKER END PLATE 2 BST AL 6061.T651 2,307.00 B A ANODIZED MIL-A-8625, TYPE II, CLASS 1 / CHROMATE, MIL-C-5541

PG110-06 A







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



STR

SA

M DOUBLE LOCKER REAR PANEL 1 BST AL 6061.T651 459.50 B A ANODIZED MIL-A-8625, TYPE II, CLASS 1 / CHROMATE, MIL-C-5541

PG110-07 A

M PHILLIPS FLAT HEAD 100° 10-32 X 3/8"

16 A&I BOLT SS 303 A A ATTACH RING TO LATCH BRACKET, VIBRATITESC10-1 A

M BUTTON HEAD CAP 3-48 X 1/4" 24 A&I BOLT SS 303 A A ATTACH REAR PANEL TO LOCKER WALLS, VIBRATITE, NO WASHER

SC3-1 A

M SOCKET HEAD CAP 3-48 X 3/8" 24 A&I BOLT SS 303 A A ATTACH RING TO LOCKER WALLS, VIBRATITE, NO WASHER

SC3-2 A

N DOUBLE SIDED TAPE - 2" WIDE 3M ACRYLIC ADHESIVE, A60

0.005 900 U U ADHERE FOAM TO SHELL, MOUNTED TO METAL STRUCTURE, ISOLATED FROM IGNITION SOURCE

950 A

N VIBRATITE ND INDUSTRIES VARIOUS 0.80 U U PREVENTS LOOSENING OF FASTENERSFORMULA 3 A

N VIBRATION ISOLATION FOAM 5 FOAM FAB./BST PYRELL 472.50 0.5 1800 B U ISOLATION OF PAYLOAD FROM SHELL, CONTAINED BY AL DOUBLE LOCKER SHELL, NOMEX COVERED

PG110-08 A

N 3M 950 PSA TAPE (DOUBLE STICKY TAPE)

1 BST ACRYLIC 0.005 < 4 SQIN EACH

JSC-RECOMMENDED FOAM ADHESIVE. BONDED BETWEEN FOAM AND FLAME BARRIER, AND BETWEEN ALUMINUM SHELL AND FOAM. FULLY CONTAINED IN ALUMINUM

PG110-XX 4

N NOMEX COVER FOR PYRELL FOAM 5 BST NOMEX 150.00 0.1 1800 A U FLAME BARRIER BETWEEN PYRELL AND PGBA INSERT AS WELL AS MECHANICAL PROTECTION / LOW FRICTION. ADHERED TO FOAM WITH 3M 950 PSA TAPE

PG110-XX 4

N INTERFACE LABEL: "PG000-00" 1 BROTHER ACRYLIC ADHESIVE 0.50 0.005 0.25 U U INTERFACE LABELS, BONDED TO METAL, NO FLAME SOURCE

PG120-XX A







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



STR

SA

N INTERFACE LABEL: "PGBA S/N-003" 1 BROTHER ACRYLIC ADHESIVE 0.50 0.005 0.25 U U INTERFACE LABELS, BONDED TO METAL, NO FLAME SOURCE

PG120-XX A




SUBASSEMBLY: FACE PLATE ASSEMBLYASSEMBLY DRAWING: PG120-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



STR

FP

M HINGE MOUNTS 2 BST AL 6061.T6 B A CHROMATE, MIL-C-5541 4

M AIR INLET SHIMSTOCK COVER 1 BST AL A

M AIR INLET SIDE WALL, LEFT 1 BST AL 6061.T6 B A CHROMATE, MIL-C-5541 A

M AIR INLET SIDE WALL, RIGHT 1 BST AL 6061.T6 B A CHROMATE, MIL-C-5541 A

M J2 BACKSHELL, ISS 1 GLEN AIR SS 14.10 A A 4

M J1 BACKSHELL, ISS 1 GLEN AIR SS 14.10 A A 4

M GSE ALIGNMENT CATCHES 2 BST AL 6061.T6 B A CHROMATE, MIL-C-5541 4

M SWITCH GUARD / HANDLE FOR CIRCUIT BREAKER, MCMASTER CARR 5/32RDX3" (1726A44)

2 MCMASTER CARR SS 303 53.40 A A1726A44, RAF P/N 8047-440-SS

4

M LATCH CATCHES 4 BST AL 6061.T6 16.00 B A ANODIZED MIL-A-8625, TYPE II, CLASS IGBA-90-034-C A

M LATCH HANDLES 4 BST AL 6061.T6 45.60 B A ANODIZED MIL-A-8625, TYPE II, CLASS IGBA-90-034-H A







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



STR

FP

M LATCH BALL BEARING 16 GFE/ LOCKHEED CRES A276 6.44 A A ATTACH LATCH CATCHESMS19060-4812 A

M FACE PLATE, ISS MODIFICATION 1 BST AL 6061.T651 1,395.69 B A ANODIZED MIL-A-8625, TYPE II, CLASS 1 / CHROMATE, MIL-C-5541

PG120-01 4

M AIR INLET FAN GUARD FRAME 1 BST AL 6061.T6 91.20 B A CHROMATE, MIL-C-5541PG120-03 A

M AIR INLET SCREEN, 24X24, 0.0075", 67.4%, 0.034" OPEN

1 BST, MCMASTER CARR

SS 304 19.00 A A MCMASTER CARR: 9230T524PG120-04 234

M AIR OUTLET FAN GUARD FRAME 1 BST AL 6061.T6 102.40 B A CHROMATE, MIL-C-5541PG120-05 A

M AIR OUTLET SCREEN, 16X16, 0.009", 71.9%, 0.053" OPEN

1 BST, MCMASTER CARR

SS 304 19.00 A A MCMASTER CARR: 9230T521PG120-06 234

M LATCH HANDLE SLEEVES 8 BST SS 303 0.60 A APG120-09 A

M LATCH SPACERS - 0.031" 4 BST AL 6061.T6 0.63 B A CHROMATE, MIL-C-5541PG120-11 A

M FLAT HEAD PHILLIPS, 2-56 X3/16" 8 A&I BOLT SS 303 0.94 A A ATTACH LATCH BASESC2-2 A

M FLAT HEAD SOCKET 4-40 X 3/8" 12 A&I BOLT SS 303 6.00 A ASC4-7 A







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



STR

FP

M FLAT HEAD CAP, 4-40 X 3/8" 8 A&I BOLT SS 303 3.20 A A ATTACH LATCH CATCHESSC4-7 A

M LATCH KNOB, RIGHT 2 GFE/LOCKHEED CRES 15-5 PH 46.04 A ASDD39119020-001 A

M LATCH KNOB, LEFT 2 GFE/LOCKHEED CRES 15-5 PH 46.04 A ASDD39119020-002 A

M LATCH BASE 4 GFE/ LOCKHEED CRES 15-5 PH 45.60 A ASDD39119021-022 A

M LATCH, BALL PLUNGER 4 GFE/LOCKHEED CRES 302 A ASS8H-54N A

M LATCH RETAINING RING 4 GFE / LOCKHEED CRES 302 2.80 A A PASSIVATEDWSM-75 A

M LATCH CATCH BALL PLUNGER 6-40 X 5/16"

8 REID TOOL SS 2.67 A AX3 A

M/N J1 COVER, TETHERED CAP, ISS 1 GLEN AIR SS 14.40 A A PROGRAM MANDATED, METAL ENCLOSURE 4

M/N SWITCH, LOCKING, TOGGLE, 2P2T, LCD ENABLE

1 NEWARK VARIOUS 42.10 U U U U MOUNTED TO STRUCTURE23F315 A

M/N FRONT PANEL VIDEO CONNECTOR 1 AMPHENOL VARIOUS, PC, STEEL 6.90 U U METAL ENCLOSURE31-10-75 234







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



STR

FP

M/N J3 VIDEO CONNECTOR, BNC FEMALE, ISOLATED, ISS

1 AMPHENOL VARIOUS: STEEL, NICKEL PLATED, PC

6.60 U U 75 OHM, ISOLATED TO CHASSIS, RENAMED J3 TO J4 FOR ISS, MOUNTED TO STRUCTURE

31-10-75 4

M/N CIRCUIT BREAKER, MAIN, 10A 1 ETA VARIOUS, ELECTRONICS ASSEMBLY

19.90 U U 10 AMP, HEAT SUNK TO STRUCTURE, AIR COOLED

483-6533 JIMI-B2507-10

1234

M/N HANDLE, CENTER, 7.25X1.5X0.375 1 ALLIED ELECTRONICS

SS, HEAT SHRINK COVER

151.20 U U HUMAN INTERFACE, MOUNTED TO STRUCTURE

543-3046 A

M/N J3 COVER, BNC MALE, TETHERED CAP, ISS

1 AMPHENOL STEEL, NICKEL PLATED

14.40 A A METAL ENCLOSURE713-1008 / 31-6 4

M/N LED, GREEN, "MAIN POWER" 1 STANLEY VARIOUS, ELECTRONICS ASSEMBLY

1.50 U UHPG5066X 4

M/N LED, GREEN, "TOUCHSCREEN ENABLED"

1 STANLEY VARIOUS, ELECTRONICS ASSEMBLY

0.30 U U CHANGED AT JSC REQUEST - HUMAN FACTORS REQUIREMENT, MOUNTED TO STRUCTURE

HPY5066X 4

M/N J2 EXPRESS DATA, ISS 1 CTI VARIOUS: STEEL, SILICONE RUBBER

28.00 U U ISS PROGRAM-PROVIDED, MOUNTED TO STRUCTURE

MS27468T15F35P 4

M/N J2 COVER, TETHERED CAP, ISS 1 GLEN AIR SS, SILICONE RUBBER 14.40 A A METAL ENCLOSUREMS27502F15CL, 06324

4

M/N J1 POWER CONNECTOR, ISS 1 ITT CANON VARIOUS: STEEL, SILICONE RUBBER

24.00 U U ISS PROGRAM-PROVIDED, ITT P/N: PV0G14B4PN16, MOUNTED TO STRUCTURE

NBOE14-4PT-4PNT

4

N LED COVER 2 NEWARK PC 0.60 U U CONTAINMENT/LIGHT DIFFUSION/MOUNTING, MOUNTED TO STRUCTURE

CLF280CTP 4







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



STR

FP

N VELCRO PILE 1 TBE NYLON HOOK, PSA 1 16 U U TEMP STOW OF COMPONENTS ON FRONT PANEL

FO-37127-IP0400 A

N VIBRATITE 1 ND INDUSTRIES VARIOUS 0.50 U U U U PREVENTS LOOSENING OF FASTENERSFORMULA 3 A

N TOUCHSCREEN ADAPTOR RING 1 BST PC 93.50 U U ELECTRIC ISOLATION TO CHASSIS, MOUNTED TO METAL STRUCTURE

PG120-07 A

N SILICONE RUBBER FOR BACKSHELL STRAIN RELIEF

1 BST SILICONE U U STRAIN RELIEFPG120-12 A

N INTERFACE LABELS, BLACK ON WHITE

6 BROTHER ACRYLIC ADHESIVE 0.50 0.005 7 U U INTERFACE LABELS, BONDED TO METAL, NO FLAME SOURCE, PER JSC HF REQUIREMENT

PG120-13 4

N DECAL, FIRE HOLE, IVA, DIA0.74" 1 NASA JSC PROV. LEXAN, ADHESIVE (467)

0.50 0.010 0.25 U U JSC-MANDATED. RESTRICTION: SHORT TERM LOW EARTH ORBIT, FLAMMABILITY

SDD32100397-001 A

N DECAL, ESD, IVA, 0.5" 1 NASA JSC PROV. LEXAN, ADHESIVE 0.50 0.010 0.25 U U JSC-MANDATED. RESTRICTION: SHORT TERM LOW EARTH ORBIT, FLAMMABILITY

SDG32104805-003 4

N DECAL, IMS LABEL, IVA, 0.5X1.0", IMS BARCODE 00012219J

1 NASA JSC PROV. HELIOSCAN(POLYESTER), ADHESIVE


SDG32105720-022 4

N DECAL, CURRENT/FUSE, IVA, 0.59X0.5"

1 NASA JSC PROV. SCOTCHCAL-220 (VINYL), ADHESIVE

0.50 0.010 0.3 U U JSC-MANDATED. RESTRICTION: SHORT TERM LOW EARTH ORBIT, FLAMMABILITY, PVC

SDG32106316-006 4

N DECAL, HAZARDOUS/NONHAZARDOUS LOGO, IVA, 1.8X1.43" '0'=-043, '1'=-055, '2'=-063

1 NASA JSC PROV. LEXAN, ADHESIVE (467)


SKD39123122-XXX A




SUBASSEMBLY: INTERNAL STRUCTUREASSEMBLY DRAWING: PG130-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



STR

INS

M FRONT PANEL STANDOFF, LOWER, 0.45X0.55X0.8", 5/16-18

1 BST AL 6061.T6 10.00 B A CHROMATE, MIL-C-5541, CONNECTS GSE BOLTS TO BASEPLATE

PG130-07 234

M BASE PLATE 1 BST AL 6061.T6 375.00 B A CHROMATE, MIL-C-5541PG130-10 234

M AFT PGC BRACKET, PGC STANDOFFS, 2X2.25X1/8"

2 BST AL 6061.T6 28.00 B A CHROMATE, MIL-C-5541, CONNECTS PGC TO STRUTS

PG131-01 234

M PGC SUPPORT ELEMENTS, CHASSIS, SIDE BRACE, DIA0.375X9.33, 0.050 WALL

2 BST AL 6061.T6 91.00 B A CHROMATE, MIL-C-5541, TUBULAR SUPPORT STRUTS

PG131-02 234

M PGC SUPPORT ELEMENTS, CHASSIS, AFT POST, DIA0.375X7.604, 0.050 WALL


PG131-03 234

M PGC SUPPORT ELEMENTS, AFT BRACE, SIDE BRACE, DIA0.375X12.828, 0.050 WALL


PG131-04 234

M PGC SUPPORT ELEMENTS, CHASSIS, FORWARD POST, DIA0.375X6.019, 0.050 WALL


PG131-05 234

M FORWARD SUPPORT GRACKET, PGC, PGBA, 6.5X3.5X1/8"

2 BST AL 6061.T6 126.00 B A CHROMATE, MIL-C-5541, CONNECTS PGC/HX TO STRUTS

PG131-07 234

M PGC SUPPORT BASE CONNECTORS, PGBA, 0.5XDIA0.28"

4 BST AL 6061.T6 1.00 B A CHROMATE, MIL-C-5541, STRUT BASESPG131-08 234

M PGC SUPPORT ELEMENTS, CHASSIS, FORWARD BRACE, DIA0.375X12.134, 0.050 WALL


PG131-08 234




SUBASSEMBLY: INTERNAL STRUCTUREASSEMBLY DRAWING: PG130-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



STR

INS

M BASE PLATE, INTERNAL, 14.325X18.875X0.225"

2 BST AL 6061.T6 82.00 B A CHROMATE, MIL-C-5541, WEIGHT RELIEF ON BOTTOM

PG131-08 234

M CLEVIS, PGBA CHAMBER STANDOFF, 0.545X1.275"

2 BST AL 6061.T6 13.10 B A CHROMATE, MIL-C-5541, END PIECE FOR TUBES

PG131-11 234

M CROSS BRACE CONNECTOR, PGC SUPPORT STRUTS, 0.5X0.5*1.5"

6 BST AL 6061.T6 97.00 B A CHROMATE, MIL-C-5541, TUBE CONNECTORPG131-12 234

M ATS SUBSYSTEM ATTACHMENT PLATE, 4.375*4.998*0.625"

1 BST AL 6061.T6 181.00 B A CHROMATE, MIL-C-5541, TEFLON ANODIZE, SS HELICOILS

PG132-01 234

M ATS TAIL SUPPORT, 2.3*0.5*0.64*0.25"

1 BST AL 6061.T6 13.00 B A CHROMATE, MIL-C-5541PG132-02 234

M INLET HYDROPHOBIC MEMBRANE MOUNT, PGBA ATS, 1.975X0.98*1.0*0.150"


M AIR SENSOR MOUNTING PLATE, 7*6.5*0.125"





SUBASSEMBLY: SILENCER KIT / MUFFLERASSEMBLY DRAWING: PG140-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



STR

MUF

M SILENCER KIT - INLET BRACE SHI-FEXPR-D5160-301, IMS BARCODE 009528J

1 BOEING AL 6061.T6 50.00 A A NEW FOR STS112, BOEING P/N 3A768SOCN683-21279-4, S/N-1001

PG143-00 4

M/N SILENCER KIT - INLET SHI-FEXPR-D5114-301, IMS BARCODE 009523J

1 BOEING AL 6061.T6, AL 2117.T4, SONEX FOAM, 3M ADHESIVE AEROSOL, SILICONE RUBBER FOAM

1,769.50 U U A A NEW FOR STS112, BOEING P/N 3A768SOCN683-21279-4, S/N-1001, METAL ENCLOSURE

PG141-00 4

M/N SILENCER KIT - OUTLET SHI-FEXPR-D5115-301, IMS BARCODE 009524J

1 BOEING AL 6061.T6, AL 2117.T4, SONEX FOAM, 3M ADHESIVE AEROSOL, SILICONE RUBBER FOAM

2,096.00 U U A A NEW FOR STS112, BOEING P/N 3A768SOCN683-21279-4, S/N-1001, METAL ENCLOSURE

PG142-00 4

N SILENCER KIT - ADHESIVE LABEL SET

1 BOEING SCOTCHCAL 220 VINYL 5.00 0.005 < 4 EA. NEW FOR STS112, MUA APPROVAL CODE 'AA', MUA RATIONALE 9110, 9203 PER SPACEHAB ASSESSMENT

PG144-00 4

N SILENCER KIT - VELCRO KIT, IMS BARCODE 009529J

1 BOEING NYLON HOOK, PSA 20.00 0.01 < 4 EA. NEW FOR STS112, LESS THAN 4", NO FLAME SOURCE, BONDED TO STRUCTURE

PG145-00 4



SUBSYSTEM: PLANT GROWTH CHAMBER

SUBASSEMBLY: PLANT CHAMBER STRUCTURE (210/260)ASSEMBLY DRAWING: PG210-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



pgc

pcs

M EDGE TREATMENT, TOP RING 1 BST AL 6061.T6 675.00 B A CHROMATE, MIL-C-5541PG261-01 234

M CORNER, BOTTOM EXTERIOR 2 BST AL 2024.T3 ALLCLAD U U ANODIZED COATINGPG261-02 234

M CORNER, BOTTOM INTERIOR LONG

2 BST AL 2024.T3 ALLCLAD 18.00 U U ANODIZED COATINGPG261-03L 234

M CORNER, BOTTOM INTERIOR SHORT

2 BST AL 2024.T3 ALLCLAD 15.60 U U ANODIZED COATINGPG261-03S 234

M CORNER, SIDE INTERIOR 4 BST AL 2024.T3 ALLCLAD 40.80 U U ANODIZED COATINGPG261-04 234

M PENETRATION, DEHUMIDIFIER/AIR INLET

1 BST AL 6061.T6 122.80 B A CHROMATE, MIL-C-5541PG261-06-01 234

M PENETRATION, WATER TRAP/AIR SAMPLER


M PENETRATION, PRESSURE RELIEF VALVES


M PENETRATION, NUTRIENT DELIVERY SYSTEM


M PENETRATION, ELECTRICAL 1 BST AL 6061.T6 5.80 B A CHROMATE, MIL-C-5541PG261-06-05 234







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



pgc

pcs

M INSERT, SHURTAB FLOATING THREAD

14 SHUR-LOK VARIOUS 30.80 U UPG261-06-06 234

M COOLING TUBE 1 BST AL 3003.0 480.00 B A CHROMATE, MIL-C-5541PG261-06-07 234

M FACESHEET, INTERIOR SIDE WALL 2 BST AL 2024-T3 ALLCLAD 220.80 B U ANODIZED COATING, HONEYCOMB COMPOSITE, NOT SUBJECT TO STRESS

PG261-06-08A 234

M FACESHEET, INTERIOR SEAM WALL

2 BST AL 2024-T3 ALLCLAD 130.50 B U ANODIZED COATING, HONEYCOMB COMPOSITE, NOT SUBJECT TO STRESS

PG261-06-08B 234

M FACESHEET, INTERIOR BOTTOM 1 BST AL 2024-T3 ALLCLAD 103.30 B U ANODIZED COATING, HONEYCOMB COMPOSITE, NOT SUBJECT TO STRESS

PG261-06-08C 234

M FACESHEET, INTERIOR DEHUMIDIFIER WALL

1 BST AL 2024-T3 ALLCLAD 95.20 B U ANODIZED COATING, HONEYCOMB COMPOSITE, NOT SUBJECT TO STRESS

PG261-06-08D 234

M FACESHEET, EXTERIOR 1 BST AL 2024-T3 ALLCLAD 618.30 B U ANODIZED COATING, HONEYCOMB COMPOSITE, NOT SUBJECT TO STRESS

PG261-06-11-01 234

M HONEYCOMB, 1/4" CELL .003" FOIL ALUMINUM

1 PANELTEC INC. AL 249.80 U UPG261-06-11-02 234

M EDGE TREATMENT, RIGHT SEAM 1 BST AL 6061.T6 29.60 B A CHROMATE, MIL-C-5541PG261-06-11-03L 234

M EDGE TREATMENT, LEFT SEAM 1 BST AL 6061.T6 29.60 B A CHROMATE, MIL-C-5541PG261-06-11-03R 234







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



pgc

pcs

M REFLECTOR PANEL, SHORT 2 BST AL 6061.T6 B A CHROMATE, MIL-C-5541PG262-03-01 234

M REFLECTOR PANEL, LONG 2 BST AL 6061.T6 B A CHROMATE, MIL-C-5541PG262-03-02 234

M CORNER BRACKETS, REFLECTOR PANEL

4 BST AL 6061.T6 B A CHROMATE, MIL-C-5541PG262-03-03 234

M ROOT COMB RETAINER BRACKET, LONG

2 BST AL 6061.T6 63.30 B A CHROMATE, MIL-C-5541PG262-03-04L 234

M ROOT COMB RETAINER BRACKET, SHORT

2 BST AL 6061.T6 52.70 B A CHROMATE, MIL-C-5541PG262-03-04S 234

M TOP FRAME 1 BST AL 6061.T6 B A CHROMATE, MIL-C-5541PG263-01 234

M FASTENERS AR A&I BOLT SS 303 A ASC 234

M FASTENERS AR A&I BOLT SS 303 A ASC 234

N ADHESIVE, MASTERBOND AR MASTERBOND EPOXY 170.00 U K ATTACHES METAL COMPONENTSEP21LV-HGS 234








MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



pgc

pcs


N ADHESIVE, MASTERBOND AR MASTERBOND EPOXY 170.00 U K ATTACHES METAL COMPONENTS, CONTAINED WITHIN PLANT GROWTH CHAMBER

EP21TCHT-1 234

N LEXAN WINDOW, OPTICAL CLEAR 1 BST LEXAN A APG263-02 234

N GASKET SEAL 1 BST SILICONE U UPG263-03 234




SUBASSEMBLY: ROOT TRAY ASSEMBLYASSEMBLY DRAWING: PG212-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



PGC

RTA

M/N AIR TUBE BOLT 20 BST PC, 316 SS 0.75 2.2 U U A A CONTAINED IN PLANT GROWTH CHAMBERPG212-11 234

N 1/4-28 TO 1/8 HOSE BARB 1 COLE-PARMER KYNAR 0.375 0.28 U AB-30704-86 234

N 1/4-28 PLUG 1 COLE-PARMER KYNAR 0.375 0.14 U AB-30706-31 234

N 0.22 MICRON PORE MEMBRANES 30 MILLIPORE MIXED CELLULOSE ESTER

.005 1.7 U U CONTAINED IN PLANT GROWTH CHAMBERGSWP-037-00 234

N NUT, ROOT PACK COMB 20 BST PC 0.8 .75 U U CONTAINED IN PLANT GROWTH CHAMBERPG212-13 234

N ROOT PACK COMB 2 BST PC 77.79 0.1250 76.4264 U A RETAINS ROOT PACKS, CONTAINED IN PLANT GROWTH CHAMBER

PG245-05 4

N AIR TUBE, ROOT TRAY ASSEMBLY 20 BST PC 183.83 0.0630 14.8751 U A CONTAINED IN PLANT GROWTH CHAMBERPG245-08 4

N AIR TUBE NUT 20 BST PC 30.31 0.0930 2.7356 U A CONTAINED IN PLANT GROWTH CHAMBERPG245-09 4




SUBASSEMBLY: AIR PLENUM, BLOWERASSEMBLY DRAWING: PG213-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



PGC

APB

M INLET RING, BLOWER 2 EBM/PABST STEEL 73.00 0.0380 30.6357 B A ZINC9566-2-4013 4

M PLATE, FAN, BASE 1 BST AL 5052.H32 230.99 0.047 225.937 B A CHROMATE CONVERSIONPG262-02-05 4

M PLATE, FAN MOUNT 1 BST AL 6061.T6 180.22 0.0630 132.1869 B A CHROMATE CONVERSIONPG262-02-06 4

M THREADED STANDOFF 4 BST AL 6061.T6, 1/4" SQUARE

3.89 0.2500 1.9278 B A CHROMATE CONVERSIONWNDR-301 4

M SUPPORT, CORNER 4 BST AL 6061.T6 50.38 0.0630 27.3054 B A CHROMATE CONVERSIONWNDR-302 4

M WALL, BACK PLANT CHAMBER 1 BST AL 5052.H32 265.17 0.0470 257.8167 B A POWDER COAT, WHITEWNDR-303 4

M WALL, RIGHT PLANT CHAMBER 1 BST AL 5052.H32 269.79 0.0470 261.0930 B A POWDER COAT, WHITEWNDR-304 4

M WALL, LEFT PLANT CHAMBER 1 BST AL 5052.H32 265.38 0.0470 257.1865 B A POWDER COAT, WHITEWNDR-305 4

M WALL, FRONT PLANT CHAMBER 1 BST AL 5052.H32 323.08 0.0470 312.5179 B A POWDER COAT, WHITEWNDR-306 4

M SUPPORT, UPPER CORNER 4 BST AL 6061.T6 12.22 0.1250 4.9014 B A CHROMATE CONVERSIONWNDR-307 4




SUBASSEMBLY: AIR PLENUM, BLOWERASSEMBLY DRAWING: PG213-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



PGC

APB

M DIVIDER, MIDDLE 1 BST AL 5052.H32 50.11 0.0470 49.2950 B A CHROMATE CONVERSIONWNDR-308 4

M BRACKET, ANGLE 8 BST AL 6061.T6 0.54 0.0630 1.1084 B A N/AWNDR-310 4

M/N BLOWER, CENTRIFUGAL 2 EBM/PABST VARIOUS, ELECTRONICS ASSEMBLY

299.00 N/A N/A U U UL94V-0, CONTAINED IN PLANT GROWTH CHAMBER

EBM-RER125DC 4

M/N FAN ASSEMBLY 1 BST VARIOUS, ELECTRONICS ASSEMBLY

U U TOP LEVEL ASSEMBLY, SEE INDIVIDUAL ITEMSWNDR-A300 4

N STANDPIPE 2 BST PC 28.87 0.1250 47.9339 U A B A N/AWNDR-309 4




SUBASSEMBLY: PLANT CHAMBER ELECTRONICSASSEMBLY DRAWING: PG214-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



PGC

PLE

M SENSOR PACK FRONT COVER 1 ZEROCASE/BST AL 1100.0 64.61 0.0400 75.4873 B A CHROMATE CONVERSIONWNDR-403 4

M SENSOR PACK REAR COVER 1 ZEROCASE/BST AL 1100.0 57.78 0.0400 65.7742 B A CHROMATE CONVERSION, CONTAINED IN PLANT GROWTH CHAMBER

WNDR-406 4

M SENSOR PACK FRONT COVER MOUNT RING

1 BST AL 6061.T6 23.22 0.0630 19.6817 B A CHROMATE CONVERSION, CONTAINED IN PLANT GROWTH CHAMBER

WNDR-407 4

M SENSOR PACK PC BOARD MOUNT RING

1 BST AL 6061.T6 26.36 0.0630 20.894 B A CHROMATE CONVERSIONWNDR-408 4

M/N SENSOR PACK, ASSEMBLY 1 BST VARIOUS, ELECTRONICS ASSEMBLY

U U TOP LEVEL ASSEMBLY, SEE INDIVIDUAL ITEMSWNDR-AE100 4

M/N SENSOR PACK PC BOARD 1 BST VARIOUS: ELECTRONCIS COMPONENTS, CIRCUIT BOARD

100.00 0.7000 UNK U U CONTAINED IN AL ENCLOSUREWNDR-E100 4



SUBSYSTEM: THERMAL ASSEMBLIES

SUBASSEMBLY: TEMPERATURE CONTROL SYSTEMASSEMBLY DRAWING: PG221-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



TH

TCS

M 1/8" MALE NPT TO T- 1/8" TUBING FITTING [V]

1 SWAGELOK SS A A 4

M 1/8" NPT TO 1/4" TUBING FITTING [J]

1 SWAGELOK SS A A 4

M 1/8" TUBE TO 1/8" TUBE ADAPTER [O]

1 SWAGELOK SS A A 4

M 1/8" TUBING PLUG [W] 1 SWAGELOK SS A A 4

M 1/8" MALE NPT TO 1/8" FEMALE NPT FITTING [U]

1 BESWICK 303 SS, BUNA-N A A 4

M CHAMBER WALL COOLANT LOOP [E]

1 BST, SWAGELOK AL 3003.H14, 1/4"OD, 0.035"WALL

B A ALODINECL-1 -> CL-5 4

M THERMAL GREASE AAVID SILICONE U UHERMOLINK 1000 234

M FIN PLATE, HEAT EXCHANGER, H20


M 1/4" OD AL TUBING, 0.035" WALL BST AL 6061.T6 B A CHROMATE, MIL-C-5541PG221-18 234

M 1/8" OD AL TUBING, 0.035" WALL BST AL 6061.T6 B A CHROMATE, MIL-C-5541PG221-19 234







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



TH

TCS

M #6 WASHERS 44 A&I BOLT SS 303 A ASC 234

M #6 LOCKWASHERS 44 A&I BOLT SS 303 A ASC 234

M 5/16 SAE TO 1/8" SWAGELOK 1 SWAGELOK SS 316 A ASS-200-1-2ST 234

M 7/16 SAE TO 1/4" SWAGELOK 3 SWAGELOK SS 316 A ASS-400-1-4ST 234

M 1/4" SWAGELOK TEES 3 SWAGELOK SS 316 A ASS-400-3 234

M/N EXPANSION VESSEL ASSEMBLY [C]

1 BST AL 6061-T6, PC, AL 5052-H32, SS, BRASS, BUNA-N, SILICONE, NICKEL, CU, AG, SN

100.00 B A FILLED WITH WATER, INTERNAL METAL STRUCTURE, SECOND LEVEL OF CONTAINMENT

IM00630 4

M/N 10-32 FEMALE TO 10-32 FEMALE COUPLING [S]

1 BESWICK 303 SS, BUNA-N 1.80 A AMF-1010-303 4

M/N MODIFIED 10-32 MALE TO 1/16" ID TUBE FITTING, WITH 2 MICRON POROUS SS INSERT [R]

1 BESWICK, BST 303 SS, BUNA-N 3.00 A AMH-1012-303 4

M/N 10-32MALE TO 1/8"TUBE FITTING [N]

1 BESWICK 303 SS, BUNA-N 2.20 A AMH-1332-303 4

M/N 10-32 MALE TO 1/8"TUBE FITTING [T]








MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



TH

TCS

M/N 1/8"MALE NPT TO 1/8"TUBE ELBOW FITTING [M]

1 BESWICK 303 SS, BUNA-N 5.00 A AMPAL-8332 4

M/N 1/8"MALE NPT TO T-1/8"TUBE ELBOW FITTING [L]

1 BESWICK 303 SS, BUNA-N 5.00 A AMPAT-8332 4

M/N COOLANT CIRCULATION PUMP ASSY (MICROPUMP SERIES 180 GEAR PUMP+LEE+BST [A]

1 BST, MICROPUMP, LEE

SS 316, ALLOY 20, TITANIUM, HASTELLOY C-276, HASTELLOY B-2, CARBON GRAPHITE,

410.00 U U U U COMMERCIAL ASSEMBLY, OFFGAS TESTED, ALL ELECTRONICS METAL-ENCLOSED

PP-0024 4

M/N LEE PRESSURE RELIEF VALVE PRRA1872020L [B]

1 LEE 303 CRES, 17-4PH CRES, 440C CRES

CONTAINED WITHIN SS PUMP HEADPRRA1872020L 4

M/N PRESSURE SENSOR, HONEYWELL MICROSWITCH, 30PSID

1 BST / HONEYWELL POLYESTER, SILICONE, FLUOROSILICONE

12.00 U UPX26-030DV 4

M/N 10-32 MALE TO 1/16"TUBE ELBOW FITTING [Q]

1 BESWICK 303 SS, BUNA-N A ASMLS-1012-303 4

N QUICK DISCONNECT PAIR [H] 1 COLE-PARMER PP U-06364-20, U-06364-40

4

N FLEXIBLE TUBING, 1/16" ID [G] 1 CLIPPARD VINYL 5.003814.5 4

N LIQUID HX COVER 2 BST PC, GLASS FILLED 149.80 U U HEAT SUNK TO STRUCTUREPG221-01-01 234

N CAVITY O-RING 2 BST VITON U UPG221-17-10 234







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



TH

TCS

N PRESSURE SENSOR, 30 PSID, WET-WET [I]

1 HONEYWELL MICROSWITCH

VARIOUS, ELECTRONICS ASSEMBLY, POLYESTER, SILICONE,

12.00 U U ELECTRONICS ASSEMBLYPX26-030DV 4

N FLEXIBLE TUBING, 1/8" ID [F] 1 COLE-PARMER PU 11.00U-95625-03 4




SUBASSEMBLY: HUMIDITY CONTROL SYSTEMASSEMBLY DRAWING: PG222-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



TH

HCS

M 1/8" MALE NPT TO 1/8" TUBE SWAGELOK ELBOW FITTING[U]

1 SWAGELOK 303 SS 4

M 1/8" MALE NPT TO 1/8" FEMALE NPT FITTING [V]

1 SWAGELOK 303 SS 4

M 10-32 FEMALE TO 10-32 FEMALE COUPLING [S]

1 BESWICK 303 SS, BUNA-N 2.20 A AMF-1010-303 4

M 1/8" NPT MALE TO 10-32 FEMALE [J] 1 BESWICK 303 SS, BUNA-N A AMPA-1810-303 4

M POROUS PLATE 1 MOTT METTALURGICAL COMPANY

SS 316 182.80 A A 0.2 UM PORE SIZEPG222-02 1234

M WATER JACKET 1 BST AL 6061.T6 391.00 B A CHROMATE, MIL-C-5541PG222-04 1234

M TEMPERATURE SENSOR ADAPTER 1 BST AL 6061.T6 B A CHROMATE, MIL-C-5541PG222-11B 234

M FRONT HOLDING FRAME BUTTON HEAD CAP 2-56X3/8"

22 A&I BOLT SS 303 5.80 A ASC2-1 1234

M CHAMBER MOUNTING CAP HEAD SCREW 4-40X3/4"

18 A&I BOLT SS 303 15.10 A ASC4-15 1234

M HX BACK PLATE FLAT HEAD CAP 4-40X1/4"

26 A&I BOLT SS 303 11.50 A ASC4-7 1234







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



TH

HCS

M HX TUBING CONNECTOR 1 SWAGELOK SS 316 A ASS-400-2-2 1234

M HX TUBING CONNECTOR 1 SWAGELOK SS 316 A ASS-400-3TTM 1234

M/N EXPANSION VESSEL ASSEMBLY 1 BST AL 6061.T6, PC, AL 5052-H32, SS, BUNA-N, SILICONE, NICKEL-PLATE, SOLDER: CU, AG, SN

0.00 U U A A NICKEL PLATED / SILVER SOLDER, CONTAINED IN POLYCARBONATE BODY

IM00630 4

M/N EXPANSION VESSEL ASSEMBLY [C]

1 BST AL 6061-T6, LEXAN, AL 5052-H32, SS, BRASS, BUNA-N, SILICONE, NICKEL, CU, AG, SN

ALODINE, NICKEL PLATEIM00630 4

M/N MODIFIED 10-32 MALE TO 1/16" ID TUBE FITTING WITH 2 MICRON POROUS SS INSERT [R]

1 BESWICK, BST 303 SS, BUNA-N 3.00 A AMH-1012-303 4

M/N 10-32 MALE TO 1/8" TUBE FITTING [O]

1 BESWICK 303 SS, BUNA-N 2.20 A AMH-1332 -303 4

M/N 10-32 MALE TO 1/8"TUBE FITTING [N]


M/N 10-32MALE TO 1/8"TUBE FITTING [T]


M/N 10-32 MALE TO 1/8" TUBING FITTING [K]

1 BESWICK 303 SS, BUNA-N A AMH-1332-303 4

M/N 10-32 FEMALE TO 1/16" NPT MALE [P]

1 BESWICK 303 SS, BUNA-N 2.00 A AMPA-1610 4







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



TH

HCS

M/N 1/8" MALE NPT TO 1/8"TUBE ELBOW FITTING [M]

1 BESWICK 303 SS, BUNA-N 5.00 A AMPAL-8332 4

M/N 1/8" MALE NPT TO T-1/8"TUBE ELBOW FITTING [L]


M/N EMERGENCY PRIMING PORT / THERMOCOUPLE ADAPTER

1 BST AL 6061.T6 12.40 B A PORT WITH FEMALE QUICKCONNECT CHROMATE, MIL-C-5541

PG222-09 1234

M/N COOLANT CIRCULATION PUMP ASSY (MICROPUMP SERIES 180 GEAR PUMP+LEE+BST

1 BST, MICROPUMP, LEE

SS 316, ALLOY 20, TITANIUM, HASTELLOY C-276, HASTELLOY B-2, CARBON GRAPHITE,

410.00 U U U U COMMERCIAL ASSEMBLY, OFFGAS TESTED, ALL ELECTRONICS METAL-ENCLOSED

PP-0024 4

M/N PRESSURE RELIEF VALVE [B] 1 LEE 303 CRES, 17-4PH CRES, 440C CRES

U U A A COMMERCIAL ASSEMBLYPRRA1872020L 4

M/N PRESSURE SENSOR, HONEYWELL MICROSWITCH, 30PSID

1 BST / HONEYWELL POLYESTER, SILICONE, FLUOROSILICONE

12.00 U UPX26-030DV 4

M/N 10-32 MALE TO 1/16"TUBE ELBOW FITTING [Q]

1 BESWICK 303 SS, BUNA-N 3.00 A ASMLS-1012-303 4

N INITIAL WATER PRIME 1 BST H20 35.90 A A 1234

N HX/BACK CENTER SCREWS O-RING

4 PORTER SEAL BUNA-N 0.10 U U#A-8 1234

N HX/SWAGELOK O-RING 2 PORTER SEAL BUNA-N 0.40 U U-15 1234







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



TH

HCS

N FLEXIBLE TUBING, 1/16" ID [G] 1 CLIPPARD VINYL 5.003814.5 4

N CONDENSATE TUBING 1/8" ID COLE-PARMER NORPRENE A AE-06410-03 1234

N CONDENSATE TUBING CONNECTOR 1/4-28X1/16"

5 COLE-PARMER KYNAR 3.00 U A 3.1 G (TOTAL)E-30708-84 1234

N RETENTION FRAME 1 BST GRAPHITE/FIBERGLASS

63.00 U UPG222-01 1234

N MAIN FRAME 1 BST PC 146.10 U UPG222-03 1234

N COVER PLATE, DEHUMIDIFIER 1 BST GRAPHITE/FIBERGLASS

111.70 U UPG222-05 1234

N HX/COVER PLATE O-RING 1 BST BUNA-N 3.20 .07 0.11 U U LIQUID SEALPG222-06 1234

N RESERVOIR, H20, HUMIDITY CONTROL

1 LIQUIBOX (MOD. BY BST)

PE, NYLON 40.00 0.01 125 U U LIQUID STORAGEPG222-08 1234

N MANIFOLD FOR MICROPUMPS 1 BST PC 30.00 U UPG222-10-1 234

N HX/MAIN FRAME O-RING 1 BST BUNA-N 3.40 .07 0.11 U U LIQUID SEALPG222-12 1234







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



TH

HCS

N HUMIDITY UNIT/CHAMBER O-RING 1 BST BUNA-N 2.70 .07 0.12 U U AIR SEALPG222-13 1234

N POROUS PLATE O-RING 1 BST BUNA-N 3.40 .07 0.11 U U AIR/LIQUID SEALPG222-14 1234

N PRESSURE SENSOR, 30 PSID, WET-WET [I]

1 HONEYWELL MICROSWITCH


12.00 U U ELECTRONICS ASSEMBLYPX26-030DV 4

N QUICK DISCONNECT [H] 1 COLE-PARMER PPU-06364-20, U-06364-40

4

N FLEXIBLE TUBING, 1/8" ID [F] 1 COLE-PARMER PU 11.00U-95625-03 4




SUBASSEMBLY: TEMPERATURE CONTROL ELECTONICSASSEMBLY DRAWING: PG223-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



TH

TCE

M BIMETALLIC SAFETY SWITCH HOT SIDE

2 TEXAS INSTRUMENTS

SS U UM113511382 1234

M BIMETALLIC SAFETY SWITCH COLD SIDE

2 TEXAS INSTRUMENTS

SS U UM221F035030522 1234

M/N PRESSURE SENSOR 1 SENSYM SS 303 107.60 A A CHAN 132030G2 (LM 335 (SEN7)

1234

M/N MICROPUMPS, 50 UL FIXED, 3%, 12VDC

3 LEE, INC VARIOUS, ELECTRONICS ASSEMBLY

136.20 U ULPLA1230350L 1234

N TECS, HUMIDITY HX 8 MELCOR CERAMIC, VARIOUS 58.32 A A HEAT SUNK TO STRUCTURECP1.0-127-06L 234

N TECS, TEMPERATURE CONTROL HX

8 MELCOR CERAMIC, VARIOUS 58.32 A A HEAT SUNK TO STRUCTURECP1.0-127-08L 234

N TEMPERATURE SENSOR, LM335, ASSEMBLY

5 NATIONAL SEMICONDUCTOR

VARIOUS, ELECTRONICS ASSEMBLY

0.20 U U U U CHAN 14LM 335 (SEN7) 1234

N PRESSURE TRANSDUCER, 1 PSID, 5 VDC, AMPLIFIED

1 DATA INSTRUMENTS


8.00 0.5 0.4 U U U U CHAN 9XCA-401DN (SEN5)

1234




SUBASSEMBLY: THERMAL CONTROL, AIRASSEMBLY DRAWING: PG224-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



TH

TCA

M FAN SHROUD 1 BST AL 6061.T6 B A CHROMATE, MIL-C-5541 234

M HX MOUNTING PLATES 2 BST AL 6061.T6 B A CHROMATE, MIL-C-5541PG224-07 234

M HX ALLIGNMENT BAR 2 BST AL 6061.T6 B A CHROMATE, MIL-C-5541PG224-08 234

M AIR HEAT EXCHANGER, FINNED, RTHETA

2 BST/R-THETA AL 1,820.00 U UPG224-09 234

M/N FAN, AXIAL, 12VDC, 3.5W, 290 MA 2 EBM/PABST AL, ULTRAMID A3XG5 758.00 u u U U COMMERCIAL ASSEMBLY, FLAME RETARDENT, METAL SHROUD, PLASTIC IMPELLER, STALL-PROTECTED AND FUSED, ULTRAMID A3XG5 (POLYAMIDE, 50%

4182NGX A



SUBSYSTEM: ATMOSPHERE COMPOSITION ASSEMBLY

SUBASSEMBLY: CARBON DIOXIDE SYSTEMASSEMBLY DRAWING: PG231-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



ATS

CDS

M BAOH CARTRIDGE 1 BST AL 6061.T6/PTFE 189.00 A A B A CHROMATE, MIL-C-5541PG231-01 234

M BAOH CARTRIDGE LID 1 BST AL 6061.T6 B A CHROMATE, MIL-C-5541PG231-02 234

M SINTERED DISC (FRIT), BAOH COMPATIBLE

2 BST SS 316 0.30 A APG231-03 234

N BARIUM HYDROXIDE, GRANULATED

1 ALLIED HEALTHCARE

BA(OH)2 200.00 U U CARBON DIAOXIDE SCRUBBING, CONTAINED IN AL ENCLOSURE

44-01-0006 234

N FILTER, GLASS, BAOH COMPATIBLE

2 BST BOROSILICATE GLASS 0.30 U U CONTAINED IN ATSPG231-04 234




SUBASSEMBLY: ETHYLENE REMOVAL SYSTEMASSEMBLY DRAWING: PG232-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



ATS

ERS

M ADAPTER, ETHYLENE REMOVAL SYSTEM

1 BST AL 6061.T6 B A CHROMATE, MIL-C-5541PG232-01 A

M #4 FLAT WASHER 4 A&I BOLT SS 316 0.80 A A ETHYLENE REMOVAL MOUNTSC4-1 A

M 1 3/4 #4 BUTTONHEAD SCREW 4 A&I BOLT SS 303 6.80 A A ETHYLENE REMOVAL MOUNTSC4-18 A

M 2 1/4" #4 BUTTONHEAD SCREW 4 A&I BOLT SS 303 10.00 A A ETHYLENE REMOVAL MOUNTSC4-19 A

M #4 LOCKWASHER 8 A&I BOLT SS 303 0.80 A A ETHYLENE REMOVAL MOUNTSC4-2 A

N PHOTOCATALYTIC UNIT (ETHYLENE SCRUBBER)

2 WCSAR PC, VARIOUS 240.00 0.875 10.72 U U TIO2, UV LAMPS, BALLASTS, MOUNTED TO STRUCTURE

FU 46 A




SUBASSEMBLY: ACTIVATED CARBON SYSTEMASSEMBLY DRAWING: PG233-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



ATS

ACS

M CARTRIDGE 1 BST AL 6061.T6 189.00 B A ACTIVATED CARBON CHROMATE, MIL-C-5541PG233-01 234

M CARTRIDGE LID 1 BST AL 6061.T6 B A ACTIVATED CARBON CHROMATE, MIL-C-5541PG233-02 234

M SINTERED DISC (FRIT), BAOH COMPATIBLE

2 PHIFIER/BST SS 316 0.30 A A CONTAINMENT 0.1UPG233-03 234

M FILTER, GLASS, BAOH-COMPATIBLE

2 BST BOROSILICATE GLASS 0.30 U U CONTAINMENTPG233-04 234

N ACTIVATED CARBON, GRANULES 1 R&D SEPARATIONS CARBON 200.00 U U HYDROCARBON REMOVAL, CONTAINED IN AL ENCLOSURE

AC-R 234




SUBASSEMBLY: WATER CONTAINMENT SYSTEMASSEMBLY DRAWING: PG234-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



ATS

WCS

M WATER TRAP 2 BST AL 6061.T6 100.00 B A WATER CONTAINMENT CHROMATE, MIL-C-5541PG234-01-1 234

M WATER TRAP COVER 1 BST AL 6061.T6 B A CHROMATE, MIL-C-5541PG234-01-2 234

M SOCKET HEAD CAP SCREWS 4-40 X 1/4"

8 A&I BOLT SS 303 A A WATER TRAP IN-LINE MOUNTSC 234

M SOCKET HEAD CAP SCREWS 2-56 X 1/2"

8 A&I BOLT SS 303 0.80 A A WATER TRAP IN-LINE LIDSC 234

N LARGE FILTER, CHAMBER AIR OUT, HYDROPHOBIC, PTFE

1 MILLIPORE PP, PVDF 140.00 2.5 98.125 U U HIGH AIR FLOWKVGB04NP3 A




SUBASSEMBLY: ATMOSPHERE CONTROLASSEMBLY DRAWING: PG235-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



ATS

ATC

M T- 1/4" TUBE TO 10-32 FEMALE FITTING [U]

1 SWAGELOK ALUMINUM 5.00 B A 4

M 1/8" NPT MALE TO 1/8" SWAGELOK FITTING [T]

1 SWAGELOK 303 SS 5.00 A A 4

M CHECK VALVE, 0.3 PSI 4 CIRCLE SEAL AL 6061, BUNA-N 163.50 B A259 A-BB-1/4"0.3 A

M AL. TUBING 75.5" BST AL 6061.T6 79.80 B APG235-03 A

M MANIFOLD/BRACKET 1 BST AL 6061.T6 181.00 B A CHROMATE, MIL-C-5541PG235-06 234

M 1/4" #6 FLATHEAD SCREW 2 A&I BOLT SS 303 1.20 A A MF #3 MOUNTSC6-3 A

M 1/4" #6 FLATHEAD SCREW 2 A&I BOLT SS 303 1.40 A A PROP. SOLENOID MOUNTSC6-3 A

M #8 LOCKWASHER 3 A&I BOLT SS 303 0.30 A A AIR PUMPSC8-2 A

M #8 LOCKWASHER 5 A&I BOLT SS 303 0.50 A ASC8-2 A

M 1/2" #8 SOCKETHEAD SCREW 3 A&I BOLT SS 303 4.80 A A AIR PUMPSC8-4 A







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



ATS

ATC

M 1/2" #8 FLATHEAD SCREW 3 A&I BOLT SS 303 4.20 A A AIR PUMPSC8-5 A

M 5/8" #8 FLATHEAD SCREW 2 A&I BOLT SS 303 1.60 A A MF #2 MOUNTSC8-7 234

M 5/8" #8 FLATHEAD SCREW 2 A&I BOLT SS 303 1.60 A A MF #1 MOUNTSC8-7 234

M 3/4" #8 SOCKETHEAD SCREW 5 A&I BOLT SS 303 10.50 A ASC8-8 A

M 3-WAY SOLENOID 2 CLIPPARD HYTREL, NICKLE PLATED BRASS AND STEEL

124.40 U U U USV-2 / ETO-3 234

M/N AIR-OUTLET-ADAPTER [AB] 1 BST AL 6061.T6 B A 4

M/N 10-32 MALE (ADJUSTABLE) TO 3X 10-32 FEMALE FITTING [N]

1 BESWICK 303 SS, BUNA-N 7.20 A AMCM-1010 4

M/N 10-32 MALE TO 10-32 FEMALE FITTING [J]

1 BESWICK 303 SS, BUNA-N 1.80 A AMEB-1010-0 4

M/N 10-32 MALE TO 10-32 FEMALE FITTING [C]

1 BESWICK 303 SS, BUNA-N 1.80 A AMEB-1010-0-303 4

M/N 10-32 MALE TO 1/4" TUBE FITTING [I]

1 BESWICK 303 SS, BUNA-N 2.50 A AMH-1004 4







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



ATS

ATC

M/N 10-32 MALE TO 1/4" TUBE FITTING [B]


M/N 10-32 MALE TO 1/8" TUBE FITTING [H]

1 BESWICK 303 SS, BUNA-N 2.20 A AMH-1332 4

M/N 10-32 MALE TO 1/8" TUBE FITTING [A]


M/N 1/8" NPT MALE TO 1/8" TUBE FITTING [R]

1 BESWICK 303 SS, BUNA-N 5.00 A AMPAH-8332-303 4

M/N 1/4" NPT MALE TO T- 1/8" TUBE FITTING [P]


M/N 1/8" NPT FEMALE TO 10-32 MALE FITTING [Q]

1 BESWICK 303 SS, BUNA-N 3.80 A AMPFAE-1810-303 4

M/N 1/4" NPT FEMALE TO 1/8" TUBE FITTING [O]

1 BESWICK 303 SS, BUNA-N 5.10 A AMPFAH-4332 4

M/N 1/8" NPT FEMALE TO 1/8" TUBE FITTING [S]

1 BESWICK 303 SS, BUNA-N 5.00 A AMPFAH-8332-303 4

M/N 10-32 MALE PLUG [K] 1 BESWICK 303 SS, BUNA-N 1.40 A AMSP-1000 4

M/N 10-32 MALE PLUG [D] 1 BESWICK 303 SS, BUNA-N 1.40 A AMSP-1000-303 4







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



ATS

ATC

M/N 10-32 MALE (ADJUSTABLE) TO T-10-32 FEMALE FITTING [F]

1 BESWICK 303 SS, BUNA-N 3.80 A AMTS-1010-303 4

M/N 10-32 MALE (ADJUSTABLE) TO T-10-32 FEMALE FITTING [M]

1 BESWICK 303 SS, BUNA-N 3.80 A AMTSB-1010 4

M/N 10-32 FEMALE QUAD BLOCK [L] 1 BESWICK 303 SS, BUNA-N 5.40 A AMX-1010 4

M/N 10-32 FEMALE QUAD BLOCK [E] 1 BESWICK 303 SS, BUNA-N 5.40 A AMX-1010-303 4

N SPONGE FILTER ASSEMBLY [AN] 1 BST PCBST-WT-001 4

N 1/8" FLEXLINE TUBING 32" COLE-PARMER NORPRENE 16.00 A AE-06410-03 234

N 1/4" FLEXLINE TUBING 74" COLE-PARMER NORPRENE 111.00 A A COULD BE SHORTENED USING ONE AIR PUMP

E-06410-07 234

N PRESSURE SENSOR, 30 PSI [AI] 1 HONEYWELL MICROSWITCH 26PCDFA6G


U U ELECTRONICS ASSEMBLYPX26-030DV 4

N FLEXIBLE NORPRENE TUBING, 1/4" ID [Y]

3' COLE-PARMER NORPRENE 111.00 U UU-06410-07 4

N FLEXIBLE TUBING, 1/8" ID [X] 1' COLE-PARMER PU 16.00 U UU-95625-03 4




SUBASSEMBLY: ATMOSPHERE ASSEMBLY ELECTRONICSASSEMBLY DRAWING: PG236-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



ATS

AAE

M 3-WIRE CABLE 22" ALLWIRE TEFLON INSULATED WIRE, 200C

17.60 U B 200°C, TEFLON INSULATED WIRE A

M #6 STANDOFF NUT 2 A&I BOLT SS 303 2.30 A ASC A

M #6 LOCKWASHER 1 A&I BOLT SS 303 0.10 A A HOLDS GROUND WIRE TO CHASISSC6-1 A

M #6 LOCKWASHER 2 A&I BOLT SS 303 0.20 A A CO2 SENSOR CHASSIS GROUNDSC6-1 A

M 5/16" #6 SCREW - BUTTONHEAD 8 A&I BOLT SS 303 4.80 A A MOUNTING CO2 SENSORSC6-4 A

M 3/8" #6 SCREW - FLATHEAD 8 A&I BOLT SS 303 6.40 A A MOUNTING CO2 SENSORSC6-5 A

M 1/2" #6 BUTTONHEAD SCREW 2 A&I BOLT SS 303 1.60 A ASC6-6 A

M #8 NUT 1 A&I BOLT SS 303 1.20 A ASC8-1 A

M 7/8" #8 CAPHEAD SCREW 1 A&I BOLT SS 303 0.80 A ASC8-10 A

M 7/8" #8 SOCKETHEAD SCREW 2 A&I BOLT SS 303 1.60 A ASC8-10 A







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



ATS

AAE

N SILICONE SENSOR BACKING 1 DOW CORNING SILICONE 2.00 U U SENSOR BACKING (ESTIMATED WEIGHT)732 A

N AIR PUMP, GILLIAN, SERIES E, 24V BLDC

1 SENSIDYNE - GILLIAN

VARIOUS, STEEL, RUBBER, ELECTRONICS ASSEMBLY

368.00 2 6 U U U U801105 A

N 1/8" ID FLEX-LINE 11" COLE-PARMER NORPRENE 5.50 A AE-06410-03 A

N 1/8" ID FLEX-LINE 42" COLE-PARMER NORPRENE 21.00 A AE-06410-03 A

N CO2 SENSOR, DIFFUSIVE 1 VAISALA AL 6061, CIRCUIT BOARD

190.00 2.6 34 U U B A COMMERCIAL ASSEMBLY, CONFORMAL COATED, 10000 PPM, AMBIENT AIR, CONTAINED IN PGBA

GMM20W-10000 4

N CO2 SENSOR, DIFFUSIVE 1 VAISALA AL 6061, CIRCUIT BOARD

190.00 2.6 34 U U B A COMMERCIAL ASSEMBLY, CONFORMAL COATED, 2000 PPM, INSIDE PLANT CHAMBER

GMM20W-2000 4

N TEMP./%RH SENSOR (WITH 12" WIRE)

1 VAISALA VARIOUS, ELECTRONICS ASSEMBLY

18.00 U U CHAN 4 / CHAN 20HUMITTER 50Y (SEN3)

A

N OXYGEN SENSOR 1 CERION VARIOUS, ELECTRONICS ASSEMBLY

25.00 0.9 8.42 U U CHAN 22KE-25 (SEN1) A

N WIRE HARNESS, 2-WIRE CABLE, BAOH SOLENOID VALVE

24" ALLWIRE TEFLON INSULATED WIRE, 200C

12.20 U B CLASS E 200C WIRE, BAOH SOLENOIDPG340-XX A

N WIRE HARNESS, 4-WIRE CABLE, WCSAR SCRUBBER


12.80 U B CLASS E 200C WIRE, PHOTOCATALYTIC UNITPG340-XX A







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



ATS

AAE

N WIRE HARNESS, 4-WIRE CABLE, AIR PUMP


12.80 U B CLASS E 200C WIREPG340-XX A

N WIRE HARNESS, 4-WIRE CABLE, AIR INTAKE SOLENOID


8.00 U B CLASS E 200C WIREPG340-XX A

N PRESSURE TRANSDUCER 1 DATA INSTRUMENTS


8.00 0.5 0.4 U U COMPRESSOR DELTA P CHAN 12XCA-405DN (SEN6)

A

N PRESSURE TRANSDUCER 2 DATA INSTRUMENTS


16.00 0.5 0.4 U U EXTERNAL PRESSURE CHAN 11XCA-430AN (SEN4)

A



SUBSYSTEM: NUTRIENT DELIVERY ASSEMBLY

SUBASSEMBLY: NUTRIENT PACKSASSEMBLY DRAWING: PG241-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



NDA

NP

N ROOT PACK, POLYPROPYLENE (NUTRIENT BAGS)

30 AMES RC / BST PP, AGAR, SALTS, AGGREGATE, WATER

4,500.00 Ø2.063 43.9516 U U GAS-PERMEABLE PP PACK, SOIL / MEDIA FILLED, WATER CONTENT 80%, CONTAINED IN PLANT GROWTH CHAMBER

PG245-06 4

N SEED INSERT, ROOT PACK 30 BST VARIOUS: PP, FELT, SEED

150.00 Ø.375 UNK U U COMMERCIAL MICROCENTRIFUGE TUBE, MODIFIED

PG245-07 4




SUBASSEMBLY: NUTRIENT DELIVERY SYSTEMASSEMBLY DRAWING: PG242-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



NDA

NDS

M 10-32 FEMALE TO 10-32 FEMALE ADAPTER [L]

1 BESWICK 303 SS, BUNA-N A A 4

M QUICK DISCONNECT [D] 1 COLE-PARMER PPU-06364-20, U-06364-40

4

M/N POROUS PLATE ASSEMBLY - SUCTION CHAMBER [A]

1 BST 303 SS, BUNA-N, AL6061.T6

A A 4

M/N 10-32 MALE TO 10-32 FEMALE FITTING [M]

1 BESWICK 303 SS, BUNA-N 2.20 A AMEB-1010-0 4

M/N 10-32 MALE TO 1/8" TUBE FITTING [N]


M/N 10-32 MALE TO 1/8" TUBE FITTING [C]


M/N 10-32 MALE TO 1/8" TUBE FITTING [I]

1 BESWICK 303 SS, BUNA-N A AMLAS-1332 4

M/N 1/16" MALE NPT TO 10-32 FEMALE FITTING [G]

1 BESWICK 303 SS, BUNA-N 2.00 A AMPA-1610 4

M/N 1/16" MALE NPT TO 10-32 FEMALE FITTING [B]

1 BESWICK 303 SS, BUNA-N 2.00 A AMPA-1610-303 4

M/N 10-32 MALE TO T-1/8" TUBE FITTING [H]

1 BESWICK 303 SS, BUNA-N A AMTAS-1332 4




SUBASSEMBLY: NUTRIENT DELIVERY SYSTEMASSEMBLY DRAWING: PG242-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



NDA

NDS

N CHAMBER-INSERT-NDS-SNAKE-ASSEMBLY [O]

1 BST PC 4

N WATER-SUPPLY-BAG, LIQUIBOX [R] 1 LIQUIBOX, AFC PE, NYLON, PTFE 100.00 0.010" 240 U U CONTAINED IN PLANT GROWTH CHAMBER 4

N 10-32 MALE TO 1/8' TUBE FITTING [P]

1 COLE-PARMER PP 4

N 10-32 MALE PLUG [Q] 1 COLE-PARMER PP 4

N LEE-MINIPUMP-MANIFOLD-ASSEMBLY [E]

1 BST PC 4

N NORPRENE TUBING 10" COLE-PARMER NORPRENE A AH-06410-02 1234

N MICRO PUMP, 50 UL FIXED, 3%, 12VDC

1 LEE, INC VARIOUS: PPS, PBT, SS302, SS430FR, SI RUBBER, EPOXY

U U U U HEAT SUNK TO STRUCTURELPLA 1220050L 1234

N PRESSURE SENSOR, 30 PSID, WET-WET [K]

1 HONEYWELL VARIOUS, ELECTRONICS ASSEMBLY, POLYESTER, SILICONE,

12.00 ELECTRONICS ASSEMBLYPX26-030DV 4

N FLEXIBLE TUBING, 1/8" ID [J] 1 COLE-PARMER PUU-95625-03 4

N PRESSURE GAUGE, 30 PSIA, 5VDC, AMPLIFIED

1 DATA INSTRUMENTS


U U U UXCA-430AN (SEN4)

1234




SUBASSEMBLY: NDS2 - AUTOMATIC GERMINATIONASSEMBLY DRAWING: PG245-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



NDA

NDS2

M NDS COVER PLATE, BLACK 1 BST POLYSULFONE 190.67 0.1880 246.0694 A K N/APG245-04 4

M NDS MANIFOLD MOUNT 2 BST AL 6061.T6 2.49 0.0630 2.0996 B A CHROMATE CONVERSIONWNDR-311 4

M/N NUTRIENT DELIVERY SYSTEM (NDS)

1 BST VARIOUS, ELECTRONICS ASSEMBLY

U U TOP LEVEL ASSEMBLY, SEE INDIVIDUAL ITEMS, CONTAINED IN PLANT GROWTH CHAMBER

PG245-00 4

M/N NDS VALVE, 3WAY, MANIFOLD MOUNT, 12 VDC

30 LEE, INC. VARIOUS: PPS, PBT, SS302, SS430FR, SI RUBBER, EPOXY

450.00 0.2800 0.5000 U U 1.26" X 0.28", COMMERCIAL ASSEMBLY, CONTAINED IN PLANT GROWTH CHAMBER, 12V

PG245-01, LHDA1223111H

4

M/N NDS PUMP, 50 UL, FIXED, 3%, 12VDC

2 LEE, INC VARIOUS: PPS, PBT, SS302, SS430FR, SI RUBBER, EPOXY

50.00 0.7500 6.5000 U U 0.75"X0.75"X2.18", COMMERCIAL ASSEMBLY, CONTAINED IN PLANT GROWTH CHAMBER, 12VDC, 50 UL, 3% ACCURACY

PG245-03, LPL1240350L

4

N NDS BASEPLATE 1 BST POLYSULFONE 279.11 0.2500 235.6276 A K CONTAINED IN PLANT GROWTH CHAMBERPG245-02 4

N BLADDER, WATER 1 AFC PTFE 194.82 0.0200 271.8422 A A N/A, CONTAINED IN PLANT GROWTH CHAMBER

SAGE2-111 4



SUBSYSTEM: LIGHTING SYSTEM

SUBASSEMBLY: VIDEO SYSTEMASSEMBLY DRAWING: PG251-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



LT

VS

M/N VIDEO CAMERA SHROUD 4 BST AL 6061.T6, BLACK POWDER COAT, WHITE DURAFLECT

80.00 0.060 12 U U B A COVERS CAMERA ELECTRONICS, BLACK POWDER COAT / WHITE DURAFLECT COAT

PG251-01 4

N VIDEO CAMERA, BOARD, HI-RES, 3.8MM LENS

4 EDMUND SCIENTIFIC

CIRCUIT BOARD, AL, ELECTRONICS COMPONENTS, CONNECTOR, GLASS

168.00 0.125 10.8 U U MIL-SPEC POTTED / CONFORMAL COATED, CONTAINED IN AL LIGHT BOX ASSEMBLY

A54-682 4

N VIDEO SWITCHER, 4X 1 BST CIRCUIT BOARD, AL, ELECTRONICS COMPONENTS, CONNECTOR

30.00 0.125 6 U U MIL-SPEC POTTED / CONFORMAL COATED, METAL COVER

PG251-03 / PG360-02

4




SUBASSEMBLY: LIGHT BOX STRUCTUREASSEMBLY DRAWING: PG252-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



LT

LBS

M INDIUM STRIPS 3 ALDRICH INDIUM 5.00 0.004 U U FOR MERCURY AMALGAMATION, NO LOADS35,730-8 1234

M PRESSURE RELIEF VALVE 1 W.A. HAMMOND DRIERITE CO.

VARIOUS 39.70 1.735 0.31 U U U U860A601 A

M BOX LID RING 1 BST AL 6061.T6 95.80 0.125 B A CHROMATE, MIL-C-5541PG252-05 A

M BRIDGE LAMP SUPPORT (3 PAIRS) 6 BST AL 6061.T6 51.60 0.25 0.96 B A CHROMATE, MIL-C-5541PG252-09 A

M LIGHT BOX BACK WALL 1 BST AL 6061.T6 313.52 B A CHROMATE, MIL-C-5541PG252-11 234

M LIGHT BOX END 2 BST AL 6061.T6 246.80 B A CHROMATE, MIL-C-5541PG252-12 234

M LIGHT BOX SIDE 2 BST AL 6061.T6 185.40 B A CHROMATE, MIL-C-5541PG252-13 234

M LIGHT SOCKET BRACKET 3 BST AL 6061.T6 45.00 B A CHROMATE, MIL-C-5541PG252-14 234

M VIDEO MOUNTING BRACKET 1 BST AL 6061.T6 32.80 B A CHROMATE, MIL-C-5541PG252-16 234

M FACEPLATE MOUNTING BRACKETS, SIDE








MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



LT

LBS

M FACEPLATE MOUNTING BRACKET, TOP


M FAN 1/4" STAND OFFS 8 BST AL 6061.T6 3.20 B A CHROMATE, MIL-C-5541PG252-19 A

M FACEPLATE SCREWS, 10-32 , 1/2" 2 A&I BOLT SS 303 3.40 A A BUTTON HEAD INC. WASHERSSC10-3 A

M LID SCREWS, 4-40 , 1/2" 16 A&I BOLT SS 303 9.60 A A FLATHEADSC4-12 A

M SIDE WALL SCREWS, 4-40 , 5/8" 8 A&I BOLT SS 303 7.20 A A SOCKET HEADSC4-14 A

M BACK WALL SCREWS, 4-40 , 5/8" 16 A&I BOLT SS 303 11.20 A A SOCKET HEADSC4-14 A

M FAN SCREWS, 4-40 , 15/16" 8 A&I BOLT SS 303 8.00 A A BUTTON HEAD INC. WASHERSSC4-16 A

M LAMP END SUPPORT SCREWS, 4-40 , 1 3/8"

6 A&I BOLT SS 303 10.20 A A INC. WASHERSSC4-17 A

M FACEPLATE SCREWS, 6-32 , 1 3/16" 14 A&I BOLT SS 303 25.20 A A FLATHEADSC6-9 A

N LM335 SENSOR ASSEMBLY 2 NATIONAL SEMICONDUCTOR


0.40 U U CHAN 6LM 335 (SEN7) A







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



LT

LBS

N BOX LID 1 BST PC 162.40 0.125 136.88 U U MOUNTED TO METAL STRUCTUREPG252-04 A

N GROMMETS 3 BST TEFLON 15.00 U B FOR CABLE FEEDS INTO BOX, HEAT SUNK TO STRUCTURE

PG252-15 A




SUBASSEMBLY: LIGHTING SYSTEM ELECTRONICSASSEMBLY DRAWING: PG254-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



LT

LSE

M/N BALLASTS, INVERTER, 28VDC, 27 WATT, MODIFIED

3 BODINE VARIOUS, ELECTRONICS ASSEMBLY

866.70 1.45 5.82 U U CONTAINS SOME SILICONE POTTING, 1 X 145, 2 X 130, AL ENCLOSURE WITH INTERNAL ELECTRONICS, HEAT SUNK TO STRUCUTRE, AIR COOLED

28F20-40E/33 1234

M/N PHOTO SENSOR ASSEMBLY 3 BST / HAMAMATSU VARIOUS, ELECTRONICS ASSEMBLY

30.00 U U POTTED, CONFORMAL COATED, ONE SENSOR PER LAMP, CONTAINED WITHIN AL LIGHT BOX ASSEMBLY

SEN13 1234

N 1 FT CABLE WIRE (TEFLON COATED)

2 ALLWIRE TEFLON INSULATED WIRE, 200C

17.00 U B 4 WIRE, 20 GAUGE 1234

N FLUORESCENT LAMPS, BIAXIAL, 27 WATT

3 G.E. LIGHTING VARIOUS, ELECTRONICS ASSEMBLY, GLASS, STEEL, PLASTIC

409.50 0.78 18.75 U U GLASS, MERCURY (5 MG), PHOSPHOR, PLASTIC, UL94V-0

F27BX/SPX41 1234

N 12VDC FANS, LOW POWER 2 MICRONEL PC 43.20 0.5 2.61 U U UL94V-0, CONTAINED IN AL LIGHT BOX ENCLOSURE

F41MM-012XK-9 1234



SUBSYSTEM: ELECTRIC ASSEMBLIES

SUBASSEMBLY: COMPUTER ASSEMBLYASSEMBLY DRAWING: PG310-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



EL

CA

M FRONT WALL 1 BST AL 6061.T6 41.50 B A CHROMATE, MIL-C-5541PG310-01 234

M LEFT WALL 1 BST AL 6061.T6 59.00 B A CHROMATE, MIL-C-5541PG310-02 234

M RIGHT WALL 1 BST AL 6061.T6 58.20 B A CHROMATE, MIL-C-5541PG310-03 234

M BACK WALL 1 BST AL 6061.T6 57.60 B A CHROMATE, MIL-C-5541PG310-04 234

M BOTTOM LID 1 BST AL 6061.T6 73.30 B A CHROMATE, MIL-C-5541PG310-05 234

M TOP LID 1 BST AL 6061.T6 73.90 B A CHROMATE, MIL-C-5541PG310-06 234

M FRAME, SIDE 2 BST AL 6061.T6 108.60 B A CHROMATE, MIL-C-5541PG310-18 234

M FRAME, TOP 1 BST AL 6061.T6 61.50 B A CHROMATE, MIL-C-5541PG310-19 234

M COVER, SENSOR INTERFACE CARD

1 BST AL 6061.T6 70.00 B A CHROMATE, MIL-C-5541PG310-XX 234

M #4 WASHERS 34 A&I BOLT SS 303 2.67 A ASC4-1 A







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



EL

CA

M #4 ELECTRICAL SCREW .300" LONG

8 JB SAUNDERS STEEL, ZN PLATED 6.04 A USC4-20 A

M #4 NUTS 8 A&I BOLT SS 303 3.82 A ASC4-3 A

M #4-40 SCREWS (3/8") LONG 34 A&I BOLT SS 303 20.40 A ASC4-9 A

M FAN GUARD, MICRONEL, CIRCULAR, 32X32X1.5MM

1 MICRONEL STEEL, CHROME PLATED

12.00 B A CHROMATE, MIL-C-5541V360X4A029 234

M/N COMPUTER VIDEO CONNECTOR 1 AMPHENOL VARIOUS, PC, STEEL 6.90 U U31-10-75 234

M/N PC104 TO COM1 RIBBON HARNESS 1 BST VARIOUS: PTFE RIBBON CABLE, PC-FILLED CONNECTOR

10.20 10 U U CONTAINED INSIDE ALUMINUM COMPUTER ASSEMBLY

PG310-07 234

M/N COM2 INTERNAL HARNESS 1 BST VARIOUS: PTFE RIBBON, CONNECTOR

9.70 10 U U ENCLOSED WITHIN ALUMINUM COMPUTER ASSEMBLY

PG310-08 234

M/N COM3 INTERNAL HARNESS 1 BST VARIOUS: PTFE RIBBON, CONNECTOR


PG310-09 234

M/N PC104 INTERNAL POWER HARNESS

1 BST VARIOUS: PTFE WIRE, CONNECTOR

11.60 U U ENCLOSED WITHIN ALUMINUM COMPUTER ASSEMBLY

PG310-10 234

M/N DIO INTERNAL WIRE HARNESS 1 BST VARIOUS: PTFE RIBBON, CONNECTOR


PG310-11 4







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



EL

CA

M/N ANALOG INTERNAL WIRE HARNESS

1 BST VARIOUS: PTFE RIBBON, CONNECTOR


PG310-12 4

M/N CAMERA CONNECTOR ASSEMBLY 1 BST VARIOUS, ELECTRONICS ASSEMBLY

4.10 U U MOUNTED TO STRUCTUREPG310-14 A

N PC104, AMPRO, UTILITY ASSY (LED,SWITCH, SPEAKER)

1 AMPRO COMPUTERS


42.70 U U CONTAINED IN AL COMPUTER BOX ASSEMBLYA60315-REV G A

N PC104 ANDI-FG CARD 1 AJECO OY INC. VARIOUS: ELECTRONICS ASSEMBLY

84.70 U U COMMERCIAL VIDEO FRAME GRABBER, 3.6X3.8X0.9", 1 WATT, CONTAINED IN AL COMPUTER BOX ASSEMBLY

ANDI-FG 1234

N LED MOUNT 1 VISUAL COMM CO. PC 0.17 U U HEAT SUNK IN METAL STRUCTURECLF 280 A

N PC104 AMPRO COREMODULE/4GE 1 AMPRO COMPUTERS

VARIOUS: ELECTRONICS ASSEMBLY

91.60 14 U U COMMERCIAL COMPUTER ASSEMBLY, 3.6X3.8X0.9", 4WATT, PC104-BUS, CONTAINED IN AL COMPUTER BOX ASSEMBLY

CM2-4GE 4

N ACCELEROMETER, 3AXIS, CROSSBOW, +/-4G, 0-100HZ

1 CROSSBOW ELECTRONICS

VARIOUS: AL HOUSING, ELECTRONICS COMPONENTS

68.00 U U ANODIZED ALUMINUM CHASSIS, 3-AXIS ACCELEROMETER ELECTRONICS INSIDE, 5VDC SUPPLY

CXL04LP3-AL 4

N PC104 ANALOG CARD, 32 AI, 4 DAC, 24 DIO, 4 DO, 4DI

2 DIAMOND SYS. EPOXY GLASS, FR4, SN, NI

96.00 14 U U COMMERCIAL DAC ASSEMBLY, 3.6X3.8X0.9", 1WATT, PC104-BUS, CONTAINED IN AL COMPUTER BOX ASSEMBLY

DIAMOND-MM-32 4

N FAN, 41X41X12MM, 12VDC, COMPUTER BOX COOLING

1 MICRONEL PC, BLACK, GLASS-FIBER REINFORCED PLASTIC

22.00 0.5 2.61 U U COOLING OF AL COMPUTER ASSEMBLY. FAN MOUNTED INSIDE ASSEMBLY, 80 MA / 1 WATT, UL/CSA MATERIALS, FLAME RETARDENT

F41MM-012XK-9 234

N PC104 VGA CARD 1 AMPRO COMPUTERS

VARIOUS: ELECTRONICS ASSEMBLY

79.00 U U COMMERCIAL FLAT PANEL AND CRT DISPLAY ADAPTER, 3.6X3.8X0.9", 0.5 WATT, CONTAINED IN AL COMPUTER BOX ASSEMBLY

MINIMODULE VFP-II

4







MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



EL

CA

N SENSOR INTERFACE BOARD, PGBA4

1 BST VARIOUS: ELECTRONICS ASSEMBLT, METAL CONNECTOR, CIRCUTI BOARD

50.00 U U CONTAINED IN AL METAL COMPUTER BOX / LID ASSEMBLY

PG310-15 4

N SOLID STATE MEMORY CONNECTOR ASSEMBLY

1 BST VARIOUS, STEEL, SILICONE RUBBER

38.40 U U CONTAINED IN AL COMPUTER ASSEMBLYPG310-16 A

N PC104 COMPACT FLASH (SAN DISK) SOLID STATE MEMORY ASSEMBLY

1 BST VARIOUS: SAN-DISK ASSEMBLY, SAN DISK INTERFACE CARD, SAN DISKS (2X), IDE WIRE INTERFACE

60.00 U U COMMERCIAL PC104 COMPACT FLASH MEMORY INTERFACE WITH TWO CF-CARDS, CONTAINED IN AL METAL COMPUTER ASSEMBLY

PG310-XX 4

N BATTERY PACK, CLOCK BACKUP 1 TADIRAN PLASTIC 26.17 U U CONTAINED IN AL COMPUTER ASSEMBLYTL5242/W 1234




SUBASSEMBLY: LCD ASSEMBLYASSEMBLY DRAWING: PG320-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



EL

LA

N TOUCH SCREEN, LCD, 128X256 PIXEL, 5VDC

1 DESIGNTECH ENGINEERING CO.


750.50 U U U U GLASS, PC, AL, STEEL, PCB, HEAT SUNK TO STRUCTURE

GTC100 A




SUBASSEMBLY: POWER ASSEMBLYASSEMBLY DRAWING: PG330-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



EL

PA

N FERRITE EMI FILTER 1 RADIOSHACK VARIOUS, FERRITE 52.40 U U UL-LISTED FLAME RETARDENT, HEAT SUNK TO STRUCTURE

273-104 A

N POWER PCB & V&I MEAS ASSEMBLY

1 BST VARIOUS, ELECTRONICS ASSEMBLY

201.70 U U HEAT SUNK TO STRUCTURE, AIR COOLEDPG330-01 A

N DIGITAL SWITCH BOARD ASSEMBLY

2 BST VARIOUS, CIRCUIT BOARD, ELECTRONICS COMPONENTS, CONFORMAL

160.00 U U HEAT SUNK TO STRCUTUREPG330-03 A

N INPUT ATTENUATOR, VICOR, 200 WATT

1 VICOR VARIOUS, ELECTRONICS ASSEMBLY, AL

81.30 U U U U 200 WATT, 18-36 VOLT COMM. GRADE, HEAT SUNK TO STRUCTRE

V1-AWW-CU A

N 5V CONVERTOR, VICOR, 75 WATT 1 VICOR VARIOUS, ELECTRONICS ASSEMBLY, AL

86.10 U U U U 75 WATT, 18-32 VOLTS, MINI-MOD COMM. GRADE, HEAT SUNK TO STRUCTURE

V1-J10-CX A

N 24V CONVERTOR, VICOR, 100 WATT



V1-J13-CX A

N 12V CONVERTOR, VICOR, 100 WATT



V1-J16-CX A

N RIPPLE ATTENTUATOR MODULES, VICOR, 200 WATT


81.10 U U 20 AMP RAM IND; COMMERCIAL GRADE (-25 - 100°C), HEAT SUNK TO STRUCTURE

V1-RAM-C1 A




SUBASSEMBLY: WIRE HARNESSESASSEMBLY DRAWING: PG340-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



EL

WH

M SOLDER ALPHA METALS TN/PB 55.00 U UAM11642 A

M/N CONNECTORS 11 NEWARK VARIOUS 422.00 U U U UD SUB SERIES A

M/N WIRE HARNESS, COM2, PC104 TO LCD

1 BST VARIOUS: 9X PTFE WIRE, CONNECTOR

75.00 U U CLASS E 200C PTFEPG340-05 A

M/N WIRE HARNESS, ETHERNET, PC104 TO FACEPLATE


50.00 U U CLASS E 200C PTFEPG340-08 4

M/N WIRE HARNESS, PC104 POWER 1 BST VARIOUS: 4X PTFE WIRE, CONNECTOR


M/N WIRE HARNESS, DO TO SWITCHER


50.00 U U NEW FOR STS112 DIAMOND MM 32 CARD, CLASS E 200C PTFE

PG340-12 4

M/N WIRE HARNESS, DI FROM FACEPLATE


75.00 U U NEW FOR STS112 DIAMOND MM32 CARD, CLASS E 200 C PTFE

PG340-14 4

M/N WIRE HARNESS, ANALOG INPUT 1 BST VARIOUS: 40X PTFE RIBBON, CONNECTOR

0.00 U U NEW FOR STS112 DIAMOND MM32 CARDPG340-16 4

M/N WIRE HARNESS, VIDEO INPUT FROM MUX TO PC104

1 BST VARIOUS: 2X PTFE COAX, CONNECTOR


M/N WIRE HARNESS, VIDEO OUT TO J3 BNC VIDEO OUT

1 BST VARIOUS: 1X PTFE RIBBON, CONNECTOR





SUBASSEMBLY: WIRE HARNESSESASSEMBLY DRAWING: PG340-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



EL

WH

M/N WIRE HARNESS, LCD POWER 1 BST VARIOUS: 2X PTFE RIBBON, CONNECTOR


N BARRIER STRIPS 7 NEWARK PHENOLIC 95.20 U U140 A

N RING LUG MULT

NEWARK VARIOUS 27.00 U UCRS-TO-1806 A

N SHIELDED WIRE ALPHA WIRE TEFLON INSULATED WIRE, 200C

1,175.00 U BTYPE E A

N STRANDED WIRE ALPHA WIRE TEFLON INSULATED WIRE, 200C

230.00 U B CLASS E, 200CTYPE E A




SUBASSEMBLY: ELECTRICAL MISCELLANEOUSASSEMBLY DRAWING: PG350-00



MATERIAL MASS[gram]

TICKNESS[ in.]

AREA[in2]



EL

EMS

N RTV 3140 DOW CORNING SILICONE 150.00 U U POTTING CONNECTORS3140 A

N RTV 3145 DOW CORNING SILICONE 150.00 U U POTTING CONNECTORS3145 A

N ALUMINUM TAPE, SELF-ADHESIVE 8 ft TESA AL 32.80 U UBDF A

N TEFLON TAPE 5 ft FURON/CHR DIV. PTFE 1.30 A K MIL. SPEC T-3-7730A - THREAD FASTENERHM-350 A

N CONFORMAL COATING CHEMTRONICS SILICONE 300.00 U U POTTING CIRCUIT BOARDSKONFORM 2000 A

N WIRE TIES 100 PANDUIT HALAR 52.80 A UPLT1M-C702 A

N SHRINK WRAP 10 ft SUMIYOMO ELECTRIC

MIL-L-23053/8 50.40 U USEMITUBE-K (KYNAR)

A

N SILICONE RUBBER PORTER SEAL SILICONE 32.50 20 U U VIBRATION MOUNTSSILCONE 50 A

N THERMAL GREASE AAVID SILICONE 10.00 U U CONDUCTING HEAT TO TECSTHERMOLINK 1000

A

N P CLAMP 40 CATAMOUNT TEFZEL 21.00 0.05 1.8 U UW4TZ-250-5-D A

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