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Human Exploration and Operations Committee Status Ken Bowersox Committee Chair July 30 th , 2015
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Page 1: Human Exploration and Operations Committee Status - NASA · Human Exploration and Operations Committee Status ... stage pyro bolt system; 10; ... Human Exploration and Operations

Human Exploration and Operations Committee Status

Ken BowersoxCommittee ChairJuly 30th, 2015

Page 2: Human Exploration and Operations Committee Status - NASA · Human Exploration and Operations Committee Status ... stage pyro bolt system; 10; ... Human Exploration and Operations

NAC HEO Committee Members

• Ms. Bartell, Shannon • Mr. Bowersox, Ken, Chair• Ms. Budden, Nancy Ann • Dr. Chiao, Leroy • Dr Condon, Stephen "Pat" • Mr. Cuzzupoli, Joseph W. • Mr. Holloway, Tom• Mr. Lon Levin • Dr. Longenecker, David E.• Mr. Lopez-Alegria, Michael • Mr. Malow, Richard N. • Mr. Odom, Jim (James)• Mr. Sieck, Robert • Mr. Voss, James

2

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Human Exploration & Operations Mission DirectorateOrganizational Structure

Public Affairs/Legislative Affairs

CommunicationsInt’l/Interagency Relations

General Counsel

Associate AdministratorDeputy Associate Administrator

Deputy AA for Policy & Plans

Chief Technologist

Chief ScientistChief EngineerSafety & Mission AssuranceChief Health & Medical Officer

Strategic Analysis & Integration

Mission Support Services

Resources Management

Space Comm & Navigation

Launch Services

Exploration Systems 

Development

Human Spaceflight Capabilities

International Space Station

Commercial Spaceflight

Development

Advanced Exploration

Systems

Space Life & Phys. Sciences

Research & Applications

• Orion• SLS• GSDO

• CoreCapabilities(MAF, MOD, SFCO,EVA)

• RPT

• System O&M• Crew & Cargo

TransportationServices

• Comm. Crew• COTS

• AES• Robotic

precursormeasurements

• HRP, CHS• Fund. Space

Bio• Physical

Science

ISS Nat’l Lab Mgt

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Major Events Since Last NAC Meeting

– One Year Crew – past 30% complete – Successful Recovery of SpaceX 6 Dragon– Loss of Progress 59P Cargo Mission– Loss of SpaceX 7 – delayed arrival of new docking adapter– Successful launch and docking ofProgress 60P Cargo Mission– Launch of Soyuz 43 crew to ISS– Daily science activity on ISS– Dragon pad abort test– Designation of NASA crews for Commercial Crew Vehicles – Continued RS-25 Engine Testing– Humans To Mars Summit

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NAC HEO Meeting Summary April, 2015

NAC HEO Committee Meeting

Monday , July 27th, 2015

Human Exploration and Operations Budget and Status UpdateHumans to MarsJoint Meeting with NAC Technology Committee

Hydrocarbon Engine DevelopmentNasa Launch Support Program OverviewTechnology development for Human Exploration

Tuesday, July 28th, 2015

HEOMD Communication StrategyExploration Systems StatusCommercial Crew StatusAsteroid Redirect Mission StatusISS Program StatusTour of JPLResearch Subcommittee StatusCommittee Discussion and Deliberation 5

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2015 2016Apr May Jun Jul Aug Sep Oct Nov Dec Jan Feb Mar Apr May

42S

8/28

9/11

183 / 18344S

9/2 3/3

9/244S

N°718TMA-18M

173 / 17346S

3/18

3/1846S

N°731MS-01

47S

5/21

5/2047S

N°720TMA-20M

34 DaysSpX-6

4/17 5/21

4/14SpX-6

29 DaysSpX-10

2/15 3/15

2/13SpX-10

30 DaysOrb-5

4/2 5/2

3/30Orb-5

178 / 17857P

4/25

PMM relocation fromN1N to N3F (Robotics) ♦

N1 berthing kit installed ♦

(PMA3) (IDA Install)

SM 8.089/14

X2 R1410/15

05/28 -06/07 07/27 -08/05 10/28 -11/03 12/24 -01/03 02/26 -02/27 05/23

Inc 43 Inc 44 Inc 45 Inc 46 Inc 47 Inc 48

SpX-6: Empty HTV5: CALETSpX-8: BEAM

SpX-9: IDA #2SpX-10: STP-H5, SAGE IP, SAGE NVP

(42S)

(44S)(44S)(44S)

N J. Williams (CDR-48) (46S)R A. Ovchinin (46S)R O. Skripochka (46S)

(47S)(47S)(47S)

MRM2 / SM Zenith

MRM1 / FGB Nadir

DC1 / MLM / RS Node

SM Aft

N2 Fwd / PMA2N2 

Zenith

N2 Nadir

N1 Nadir

Dock

Berth

Port Utilization

Crew Rotation

Stage EVAsStage S/W

Soyuz Lit Landing

Launch Schedule

Solar Beta >60External Cargo

04/15 05/19 06/11 07/1705/23 07/21

R S. Volkov 183 days

(42S)↓(42S)↓

10 day direct handoverE A. Mogensen (44S)↑

R S. Volkov (44S)↑R A. Aimbetov (44S)↑

4/2859P

N°426M-27M

59PLost on ascent

N T. Virts (CDR-43) 200 days (41S)E S. Cristoforetti 200 days (41S)R A. Shkaplerov 200 days (41S)

200 / 20041S

6/11

N S. Kelly (CDR-45/46) (1 Yr Crew) 342 daysR M. Kornienko (1 Yr Crew) 342 daysR G. Padalka (CDR-44) 168 days

SpX-7: IDA #1

06/14 07/2108/12

08/16

N T. Kopra (CDR-47) 142 days (45S)E T. Peake 142 days (45S)R Y. Malenchenko 142 days (45S)

12/1545S

N°719TMA-19M

142 / 14245S

12/15 5/5

2/1263P

N°432MS-02

170 / 17063P

2/12

168 / 168

R-41

8/10 (PMA3)

7 day direct handover

7/360P

N°428 M-28M

139 / 13760P

7/5 11/19(34 orb)

9/2161P

N°429 M-29M

79 / 7961P

9/21 12/9

(Early GMT)

N K. Lindgren 153 days (43S)J K. Yui 153 days (43S)R O. Kononenko 153 days (43S)

7/2243S

N°717TMA-17M

153 / 15343S

7/23 12/11

12/22

9/2SpX-8

30 DaysSpX-8

9/4 10/4

12/5SpX-9

30 DaysSpX-9

12/7 1/6

R-42

6/28SpX-7

SpX-7

11/2162P

N°431 MS-01

151 / 14962P

11/23 4/20(34 orb TBD)

(Early GMT)

8/16HTV5

37 DaysHTV5

8/20 9/26

178 / 17858P

8/14

Lost on ascent

(9/12 GMT Landing)

12/3Orb-4

60 DaysOrb-4

12/6 2/4

(TBD)

♦ IDA #2 installed on PMA2

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43 Soyuz Launch/Increment 44July – December 2015

Vehicle: 43 SoyuzLaunch: July 22, 2015 (planned 4 orbit rendezvous)Docking: July 23, 2015Undock/Landing: December 22, 2015

42 Soyuz crew

Genady Padalka, Soyuz and Increment 44 CommanderScott Kelly, Increment 45/46 CommanderMikhail Kornienko, Flight Engineer

8

43 Soyuz Crew

Oleg Kononenko , Soyuz CommanderKjell Lindgren, Flight EngineerKimiya Yui, (JAXA) Flight Engineer

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Total ISS Consumables Status

9

T1: Current Capability T2: Current Capability + HTV5

Consumable – based on current, ISS system status Date to Reserve Level Date to zero supplies Date to Reserve Level Date to zero supplies

Food – 100% October 22, 2015 December 06, 2015 November 20, 2015 December 31, 2015

KTO October 13, 2015 November 27, 2015 December 04, 2015 January 15, 2016

Filter Inserts June 05, 2016 July 20, 2016 November 10, 2016 > December 31, 2016

Toilet (ACY) Inserts February 10, 2016 April 03, 2016 February 10, 2016 April 03, 2016

EDV + TUBSS (UPA Operable) March 08, 2016 June 21, 2016 March 08, 2016 June 21, 2016

Pre-Treat Tank December 11, 2015 January 22, 2016 December 11, 2015 January 22, 2016

Water (Nominal Usage) December 06, 2015 March 17, 2016 January 30, 2016 May 21, 2016

Consumable - based on system failure

EDV + TUBSS (UPA Failed) November 26, 2015 January 09, 2016 November 26, 2015 January 09, 2016

Water, if no WPA (Ag & Iodinated) October 15, 2015 December 17, 2015 November 22, 2015 January 22, 2016

O2 if Elektron supporting 3 crew & no OGA September 02, 2015 December 15, 2015 September 02, 2015 December 15, 2015

O2 if neither Elektron or OGA July 31, 2015 September 22, 2015 July 31, 2015 September 22, 2015

LiOH(CDRAs and Vozdukh off)

~0 Days ~14 Days ~0 Days ~14 Days

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Progress 59P Anomaly

Launch of 59P occurred on April 28th but failed to reach proper orbit

Most telemetry lost and attempts to activate and gain control of Progress unsuccessfulReentered on May 8, 2015

Russian commission formed to investigate failure, determine cause, provide recommendations – Alexander Ivanov, First Deputy Head Roscosmos as chair 10 versions analyzed, reduced to 1 most probable cause

NASA formed independent team to review the anomaly, partners participated – similar to 44P investigation, detailed fault tree analyses aligned with Russian findingsMost probable cause findings

Commission Report : “Design feature of the Soyuz-2 .1a LV Stage 3-to-Progress M cargo vehicle stack, related to its structural response, which resulted in the LV oxidizer and fuel tank pressure integrity breach and damage to the Progress vehicle”NASA Assessment : “Engine shutdown oscillations coincided with integrated vehicle longitudinal structural eigenmode as a dynamic interaction to cause structural failure

One possible failure scenario

structural failure resulted in oxidizer integrity breach after engine shutdown (shutdown is rapid, significant propellant remaining in tanks, large accelerometer spike reflected in data due to “hammer” effect)Resulting pressure loads on fuel tank calculated at 167MT of force, enough to result in mechanical separation of Progress with 3rd stage pyro bolt system

10

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Progress 59P Anomaly

After each flight, Rocket & Space Center Progress analyzes the actual loads, including a comparison and verification of the structural response during ascent with the pre-flight analysis and previous flights dynamic interaction upon engine shutdown not seen on FG/U 3rd stage configurations

No changes have been introduced into the Soyuz FG 43S launch vehicle systems configurationSuccessful 60P launch with Soyuz U 3rd stage on July 2nd (nominalperformance)Russian teams recently completed modal testing of the 2.1a / Progress configuration, analyses in workPlan to utilize the 2.1A 3rd stage for 62P in November (modal survey results and subsequent mods dependent) No restrictions in place for other missions utilizing the 2.1A 3rd stage

No planned crew missions on the 2.1a configuration thru 2020

11

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SpaceX-7 Mission Anomaly

SpX-7 successfully launched on time at 9:21am CT on 6/28/15At 139 seconds, the Falcon launch vehicle experienced an anomaly that ended in loss of vehicleSpaceX is leading the investigation with FAA oversightNASA supporting with LSP, CCP, and ISS Program personnel

Team collocated in Hawthorne, daily status meetings, independent assessments being performed by LSPExcellent sharing of information

Detailed fault tree developed with emphasis on second stage operation and performanceDetailed timeline (to the msec’s) developed, taking into account video lag, sensor to computer latency, etc. to correlate timing of eventsComplete audit underway of as flown configuration, reviewing preflight approved issue tickets, component level acceptance packages, integrated stage testing results, etc.

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SpX-7 Lost Cargo Summary

Crew Supplies 690 kg 92 Food BOBs, 2 Bonus Food Kits, 2 Fresh Food Kits

Crew Provisions, Crew Care, ODF

Utilization 573 kg CSA: Vascular Echo Exercise Band

ESA: Circadian Rhythms, KUBIK EBOXes, Interface Plate, EPO Peake, BioLab, Spheroids, EMCS RBLSS, Airway Mon. LiOH CartridgeJAXA: Atomization, Biological Rhythms, Multi-omics, Cell Mechanosensing3, Plant Gravity Sensing3, SAIBO L&M, Space Pup, Stem Cells, MSPR LM, Group Combustion CameraUS: 2 Polars, 6 DCBs & Ice Bricks, 1 MERLIN, FCF/HRF Resupply, HRP Resupply [Kits, MCT, Microbiome, Twin Studies], IMAX Camera, Meteor, Micro-9, MSG resupply, Nanoracks Modules & 0.5 NRCSD #7, Universal Battery Charger, Veg-03, Microbial Observatory-1, Microchannel Diffusion Experiment, Wetlab RNA Smartcycler, SCK, Story Time, MELFI TDR Batteries

Computer Resources 36 kg Proj. Screen, Sidekick, OCT Laptop & Pwr. Supply,

32GB MicroSD Cards, Generic USB Cables & PwrModules & Card Readers, Preloaded T61p Hard Drives, CD Stowage Container, Network Attached Storage Devices, XF305 Camcorders, RS-422 Adapter Cable

Vehicle Hardware 462 kg

CHECS CMS: HRM Watches, Bench Lock Studs, Glenn Harness for Kelly, Kopra, and PeakeCHECS EHS: CO2 Monitoring Assys, Filter Assys, CSA-CP/CDM Battery Assys, SIEVE Cartridge Assys, Water Kit, Petri Dish PacketsCHECS HMS: IMAKs, Oral Med PacksC&T: C2V2 Comm unit (and HTV5 Unit Data Converter)ECLSS: 3 Pretreat Tanks, Filter Inserts, 9 KTOs, UPA FCPA, CDRA ASV, IMV Valve, Wring Collector, Water Sampling Kits, OGS ACTEX Filter, ARFTA Brine Filter Assys, O2/N2 Pressure Sensor, NORS O2, 3 PBA Assys, 2 MF Beds, 2 Urine Receptacles, Toilet Paper Packages, H2 Sensor, Ammonia Cartridge Bag, PTU XFER HoseEPS: 2 Avionics restart cablesMakita Drill, PWD Filter, N3 Bulkhead Connectors, Yellow/Red Adapters, IWIS Plates, 6.0 & 4.0 Waste Xfer Bags, BEAM Ground Straps, JEM Stowage Wire Kit

EVA 167 kg SEMU, REBA, EMU Ion Filters (4), Equipment

Tethers, Gas Grap, EMU Mirrors, Crewlock Bags, SEMU arms / legsLindgren / Yui ECOKs & CCAs, Lindgren LCVGKelly LCVG, Padalka EMU Gloves

RS Cargo – RS Torque WrenchUnpressurized Cargo: IDA #1 (OB) 526 kg

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14

Orbital-4 Mission Status

Mission Planning Orbital has contracted with United Launch Alliance (ULA) for an Atlas V launch of Cygnus

First use of Atlas V401 with the Cygnus spacecraftIntegrated Mission Review (IMR) #1 was conducted on 4/9/15 with IMR #2 planned for 7/14/15Integrated Ground Processing Technical Interchange Meeting (TIM) was completed on 5/20/15Trilateral Joint Operations Panel (JOP) was conducted on 5/27/15; planning for a 60 day berthed capabilityCargo Integration Review (CIR) is planned for 7/29/15; upmass cargo capability is 3,513 kgOn track for late November/early December launch

Pressurized Cargo complement Final ISS cargo manifest will be due in Jul at Launch minus 5 (L-5) months

Unpressurized Cargo Cubesats manifested on this mission; scheduled post ISS departure

for deployment operations Cygnus Status

First enhanced Cygnus with a longer Pressurized Cargo Module (PCM)and ultraflex solar arraysFinal Integrated Systems Test (FIST) began on 6/27/15PCM was shipped to the Cape on 6/23/15 with arrival to theCape on 8/7/15Service Module planned to be completed in Aug with shipmentto the Cape in Oct

Atlas V 401 Serial Interface Test was completed on 4/22/15

Orb-3 Mishap Investigation Report provided by Orbital ATK to the FAA last week

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NAC HEO Research SubcommitteeJuly 20, 2015 – Meeting Highlights

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Review: Research Plan for Space Biology and Physical Sciences

• Draft Research Plan sent to the RS for review and comment prior to the July 20 meeting – edits provided by RS members individually

• Presentations at the meeting described the goals and plans for the research areas at five‐ and ten‐year horizons.  Committee provided feedback in extended dialog with the SLPSRAD staff

• Two major issues noted by the RS during the review: 1) Stature of the scientific community drawn to ISS research, 

and quality of the selected research, is impressive2) Crew time to implement labor‐intensive fundamental research 

is greatly curtailed in NASA’s plans.  SLPSRAD estimates that only ~2% of projected crew research time will be devoted to space biology or physical science investigations w/o additional collaboration/alignment with CASIS and HRP; these are being 

explored currently

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ISSUE: ISS Crew Time for NASA Research

Increment 45/46 (September 2015 – Marc  h 2016) Crew Time Research Plan 15 April 2015

NASA/CASIS Research Plan: Prime Requested

Prime Adjusted 

National Lab (NLO) / CASIS 389.26 291.75

NASA Research ‐ HRP 414.32 289.40

NASA Research ‐ Non HRP 1 314.34 0.00

Tech Demo 83.41 6.00

Cold Stowage 40.75 40.75

Other IP Agreements 3 25.41 25.41

Totals 1267.49 653.31

Total NASA Allocation: ‐‐ 652.50

Conclusion: Crew time allocations are severely limiting Space Biology and Physical Science’s ability to implement the guidance of the National Research Council and to support NASA’s strategic objective for the ISS: “Conduct research on the International Space Station (ISS) to enable future space exploration, facilitate a commercial space economy, and advance the fundamental biological and physical sciences for the benefit of humanity” – NAS  A 2014 Strategic Plan, Objective 1.2 

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Exploration Systems Development StatusNASA Advisory CommitteeJuly 27, 2015

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19

2015 2018J F M A M J J A S O N D

ENTERPRISE

HEO / ESDGSDO

SLSOrion

VAB HB3

Dsgn-to Sync

Build-to Sync K/O

CDRK/O

NASA ESDChart Updated: 06/18/2015

CDRBoard

CDRK/O

CDRK/O

CDRBoard

CDRBoard

ESA SMCDR (U/R)

MIR

2016 2017J F M A M J J A S O N D J F M A M J J A S O N D J F M A M J J A S O N D J F M A M J J

2019

EM-1 Uncrewed

Launch Readiness Window

AgencyFRR

IntegrationReview

VAB StackingSAR/ORR

SOPE &Lndg & RecovSAR/ORR

ITCO/PadSAR/ORR

BoosterDCR

StagesDCR

PAD39B

LM

Torino

ITL

MAF

SSC B-2

ATK

ULA

O&C

MAFCore Stage

AREngines

Boosters

LAS

SLS S/W

MSA/LVSA

ICPS

CM

ESA SM

Ground

Orion S/W

MSFC

SIL

ELEMENT LOCATION

Primary StructureComplete   

CM Structure Delivery to O&C

Press Proof Test   

CM  Prop  ProofLeak Test    IPO

Struct AssyComplete   

Pre‐IntegComplete   

ESM Integration TRR

European Testing Complete   

ESM IntegComplete

ESM Delivery to O&C

CSM to Plumbrook for T‐VacCSM to O&C

CSM H/O to Gnd Ops

30D

LAS & OgiveMfg. Start   

LAS & OgiveDel. to LASF   

MSA Delivery to Gnd Ops(to LASF – see above)

MSA & LVSA Flight Production Complete   

MSA Flight UnitProduction Start

Flight EngineDeliveries to MAF

Engine ControllerDelivery

VAC Acceptance (U/R)   

STA Manf.Complete  

CS Final MA&OComplete  

Core Stage to SSC

Green RunHotfire (U/R)

KSC/JSC

KEY:

Completed milestone

Future milestone

Change from previousreport

Delivery Milestone

(U/R) Under Review

For comments [email protected]

ESA SM STA to Plumbrook

ESA SM S/WEmulator Delivery

QM‐1 Test QM‐2 Test

Core Upgrade Complete (ITL‐01)

Power/C&DHComplete (ITL‐02)

SLS S/W Emululator. Delivery to MPCV/GSDO

MPCV S/W EmulatorDelivery

First FlightWeld on PV

Critical Path(Primary, SecondaryTertiary)Not on Critical Path

MPPF

GSDO SCCS 3.0 Validation Complete(Haz Ops C&C S/W)

ML Structural Mods Complete

VAB Platform Mods Comp.

Pad Flame Trench/Deflector Mods Complete

VABReady

MPPFReady

GFASTReady

MLReady

PadReady

B‐2 Test Stand ActivationComplete

LVSA Flight UnitProduction Start

LASF

ICPS H/O to Gnd Ops

Fwd, Center,       & Aft Segments on Dock

Aft Skirts on Dock

Core Stage Delivery to Gnd Ops 

Boosters Elementsto VABfor Stacking

Core Stage Stackingthen Partial Modal Testthen ICPS & Orion Stackingthen Full Modal Test

LVSA Delivery to Gnd OpsRoll‐out #1and DRT

WDR

Final Close‐outs & Ordnance Install

Roll‐out #2

Final Pad Ops

ICPStoVAB

LAS,CM/SMMSAtoVAB

CM/SM Mate to LAS

SIL Build‐upComplete

SIL CertS/W Rel. 12 (Green Run)

S/W Rel. 13(Flight)

S/W Rel. 14(Flight) Contingency

S/W Rel. 15(Flight) Contingency 

S/W Regression Complete

Vehicle Cert

Core StageAssy. Joined

Start Flight Motor Segments

Complete Flight Motor Segments

Flight Unit Production Start

Flight Unit Production Complete

STA Production Complete

LVSA STA Delivery

Dev. Testing Complete  

Flight IntertankAssy. & Manf. Complete

Flight Engine Section Assy. Complete

Subsystem Integ. Complete (ITL‐03)

CSM IntegrationComplete (ITL‐03)

External Interfaces Complete (ITL‐04)

Final FSWRelease

MCCReady

Post‐Flight CM Transport& Deservicing (EM‐1)

Post Flight Assessment& Review (PFAR)

BFF

RPSF

PB

O&C

MPPF

Program ControlledMilestone

FWD Assemblies on Dock

ML/VAB M‐EV&V Complete

ML/PAD M‐EV&V Complete

Umb.InstallComplete

SCCS4.0 Rel.

JM FabStart

ACM Mass Sim. Start

AM MassSim. Start

JM Del. to KSC

ACM MassSim. Del.to KSC

AM MassSim. Del.to KSC

Build-to Sync Board

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Integrated Test Lab Mockup, Denver, Colorado

EM-1 Pathfinder First Weld at Michoud Assembly Center

Crew Module Structural Test Article arrives at GRC

EM-1 Flight Aft Bulkhead EM-1 Flight Barrel machining EM-1 Flight Tunnel

Orion Accomplishments

20

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The RS-25 engine fires up at the beginning of a 500-second test June 11

On May 13, a major milestone in its preparation for testing the core stage

Hydrogen burn-off igniter test is conducted May 5 at the Redstone

21

Crews complete a 250-foot-long metal canopy for NASA's Pegasus barge.

At the Promontory, Utah test facility of Orbital ATK, the booster for NASA’s Space Launch System rocket was fired for a two minute test on March 11

Space Launch System Accomplishments

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The first work platforms have been delivered to the VAB

The first work platforms have been delivered to the VAB

The Orion Service Module Umbilical (OSMU) is being installed at the Launch Equipment Test

Facility. Testing begins in August

Ground Systems Accomplishments

Testing of the Aft Skirt Electrical Umbilical (ASEU) was successfully

completed at the Launch Equipment Test Facility in June

Testing of the Aft Skirt Electrical Umbilical (ASEU) was successfully

completed at the Launch Equipment Test Facility in June

Upgrades and modifications to the 175-ton crane are complete; the crane has been placed back

to its original position

Mobile Launcher structural modifications are complete. Ground

subsystem installation contract award planned for August 22

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National Aeronautics and Space Administration

Commercial Crew Program Status

NAC HEO CommitteeJuly 2015

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Overview

• The Commercial Crew Program (CCP) is an essential element of the the broader strategy to achieve our nation's goals in space.

• CCP will re-establish the capability to launch astronauts from US soil.• CCP will increase the ISS crew time available for research by an amount

equivalent to one additional astronaut dedicated to research.– This is critical to accomplishing the human research required for deep

space exploration during the lifetime of ISS• Commercial transportation is vital to expanding the commercial market

for low Earth orbit services, enabling NASA and its international and commercial partners to extend human presence into the solar system and to the surface of Mars.

24

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Summary

25

• CCP remains committed to supporting our Space Act Agreement partners as they advance their concepts

• Both Boeing and SpaceX are advancing their CCtCap designs• Hardware is actively being built and tested to inform design• CCP is engaged in meaningful insight with the providers• Important design challenges remain for both providers• CCP is preparing for the flight phases of the program

Boeing: Test 1 Water Landing and Rotation to Stable 2SpaceX: Pad Abort Test Static Test Firing

CCP is now at the point where all the preliminary work through the previous phases of the program is all paying off, and our two partners are off and running with effective NASA insight/oversight. We need to keep up the momentum with adequate funding to achieve safe, reliable, and cost effective commercial crew transportation services.

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Budget Status

• NASA FY2016 President’s Budget Request for CCP is $1.243B.• Fixed price, FAR-based contracts are in place• Both companies have demonstrated good progress and performance• Ending U.S. reliance on Russia for crew transportation is a priority

• While some CCtCap milestones may move from FY 2016 to FY 2017, this does not correspond to a reduction in NASA's FY 2016 funding requirements from the President's Budget Request.

• Milestones must be funded (obligated) prior to the contractor beginning work on the milestone.

• At this point, and given all the current milestone changes, NASA still requires the full CCP President's Budget Request for FY 2016.

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Budget Implications

• Near-Term– If the Agency is funded with a Continuing Resolution for the first quarter

of FY 2016, NASA will need to address how it will fund our partners’ development activities at the current contractual schedule.

• Longer-Term– If NASA does not receive sufficient funds in FY 2016 to maintain the

current schedules, the contractors will have to stop work or work at risk until additional funding can be obligated.

– In that case, the existing CCtCap contracts will need to be renegotiated, most likely resulting in schedule delays and increased contract costs.

– NASA will need to continue to rely on Russian Soyuz capability to meet America’s requirements for crew transportation services.

• NASA has no plans to downselect the number of partners in response to lower-than-requested funding levels. As experience has shown with cargo, NASA’s plan to establish a redundant crew transportation capability is critically important for robust, safe ISS operations.

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National Aeronautics and Space AdministrationHEOMD Response toNAC HEO Committee Finding Regarding “Domestic Hydrocarbon Rocket Main Engine”

28

Bill Hill, Dep AA Exploration Systems DivisionJim Norman, Director Launch Services27 July 2015

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National Aeronautics and Space AdministrationNotes from Hydrocarbon Engine and LSP Overview

• NASA is participating and offering support for the Nation’s effort to develop a new hydrocarbon engine.

• NASA is not limited in use of Russian engines for NASA missions.

• Limitations on use of Russian engines for other user’s payloads could affect costs of future NASA missions.

• Current missions under contract using RD 180 are fixed price, and should not be affected.

• Launch Support Program has formal launch readiness input for NLS launches• Advisory role for CRS• NASA Role for launch decisions on future Commercial Crew Flights still being defined but 

expected to be greater than for CRS and NLS, but reduced from SLS/Orion type program• HEO committee requesting more information from the CRS program on the launch 

readiness process to be presented at a future committee meeting.

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National Aeronautics and Space Administration

Dr. Alotta TaylorDirector, Strategic Integration and Management Division,

Human Exploration and Operations Mission Directorate (HEOMD)

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HEOMD Communications Goals

HEOMD Communications Goal 1: Enhance public and Congressional recognition of the value of human space exploration and understanding of the capabilities-driven approach in our pursuit of sending humans to Mars.

Strategies

1. Mobilize the NASA workforce to serve as knowledgeable and excited ambassadors.

2. Articulate the challenges, risks, and benefits of human space exploration; communicating in terms meaningful to our stakeholders and always delivering a call to action.

3. Leverage milestones and activities as proof points, citing the capabilities-driven approach, in our advancement towards reaching Mars with humans.

4. Cultivate and maintain relationships with opinion leaders and influencers.

5. Partner with industry and academia to expand capabilities and broaden message dissemination.

6. Proactively collaborate with Public Affairs and the Office of Legislative and Intergovernmental Affairs to ensure they are fully equipped to achieve HEOMD communications goals.

31

HEOMD Communications Goal 2: Enhance public awareness of the marvels associated with the International Space Station and its role in advancing human space exploration.

Strategies1. Incorporate the International Space Station (ISS) into the public’s

everyday consciousness.

2. Articulate the benefits to humanity, world-class research opportunities, and the role the ISS plays as a proving ground in sending humans to Mars; communicate in terms meaningful to our stakeholders and always delivering a call to action.

3. Leverage milestones and activities as proof points, citing ISS as a proving ground, in our advancement towards sending humans to Mars.

4. Cultivate and maintain relationships with opinion leaders and influencers.

5. Partner with industry and academia to expand capabilities and broaden message dissemination.

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Facebook

Facebook FollowersAccount

NASA 11M

The White House 4M

U.S. Navy 2.1M

Air Force 2M

ISS Facebook 1.8M

Kennedy 1M

Curiosity 1M

SpaceX 878K

Goddard 785K

JSC 601K

Orion 369K

Marshall 81K

Twitter

Twitter Account Followers

@NASA 10.8M

@TheWhiteHouse 6.47M

@MarsCuriosity 1.93M

@SpaceX 875K

@NASAKennedy 850K

@USNavy 491K

@NASA_Astronauts 393K

@NASA_Johnson 343K

@NASAGoddard 250K

@ISS_Research 238K

@NASA_Orion 202K

@Space_Station 174K

@NASA_Marshall 104K

Instagram

Instagram FollowersAccountnatgeo

nasa

Nasagoddard

iss

Usnavy

nasajohnson

Nasakennedy

Nasa_marshall

23.8M

3.4M

843K

595K

126K

41.4K

21.8K

17.9K

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NASA CommunicationsConference, Large-Scale Events and Exhibits

FY2015 CLEE Events

Event Location Event Date

SXSW Austin, TX 03/13-17/15

Earth Day Nat’l Mall –Union Station Washington, DC 04/18 - 22/15

World Science Festival/Fleet Week New York, NY 05/22-30/15

San Mateo Maker Faire San Mateo, CA 05/16-17/15

Comic-Con San Diego, CA 07/9-12/15

Essence Festival New Orleans, LA 06/29 -07/06/15

World Maker Faire, NYC

Balloon Fiesta

Bay Area Science Festival

CA Science Center Endeavour Fest

New York, NY

Albuquerque, NM

San Francisco, CA

Los Angeles, CA

09/26-27/15

10/2-10/15

10/24

11/15 (TBC)

FY2016 CLEE Event Recommendations

Total number of events submitted: 79

Total number of unique events submitted: 67

Events identified by multiple submitters:• NFL SuperBowl 2016 (2)• AARP Life@50+ (2)• SXSW (2)• Comic-Con San Diego (2)• Albuquerque Balloon Fiesta (2)• Earth Day at the National Mall & Union Station (3)• Oshkosh or Spirit of St. Louis Air Show (6)

Events by Target Audience:• Non science technology attentive (29)• Science and technology interested public (11)• Space and aviation enthusiasts (9)• Technology savvy; early tech adopters/influencers (5)• STEM attentive students (4) • Other – Non CLEE audiences (9)

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HEO Communications Strategy

34

• Communicate as widely as possible

• Build communities of fans & followers

• Transform them into advocates, ambassadors, creators, & collaborators

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HEO Committee Finding

Proposed NASA Human Exploration and Operations Committee Finding

Name of Committee: Human Exploration and Operations CommitteeChair of Committee: Mr. Ken BowersoxDate of Public Deliberation: July 27, 2015 (HEO Advisory Committee)

Short Title of Finding: Communication Strategy for Exploration Plans

Finding: The Committee noted a positive improvement in NASA’s effort to communicate plans for Pioneering Space, including the Journey to Mars. Because of the critical importance of public engagement in the human exploration program, the committee plans to request future briefings on this topic to monitor progress. During briefings on this topic, the committee members thought that the following aspects of the communication approach were especially important:

1. The existence of a formal strategy to guide communication efforts2. Engagement of the public using the latest communication methods including social

networking.3. Engagement of the public in new forums4. Collection of data to evaluate the effectiveness of communication efforts

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H2MMinimal Architecture

H u m a n J o u r n e y t o M a r sThoughts on an Executable Program

Firouz N a d e r iH o p p y P r i c eJohn B a k e r

Jet Propulsion Laboratory

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Building Blocks of a Minimal Architecture

Launch In‐Space Propulsion Crew Quarters

Mars SurfaceElements

Orion100KWSEP Tugs

EUSHabitat

SLS

20tMarsLander

20tLandedInfrast.

Module(S)In‐space ChemicalStages

37

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H2MMinimal Architecture

Notional Timeline20

1520

1620

1720

1820

1920

2020

2120

2220

2320

2420

2520

2620

2720

2820

2920

3020

3120

3220

3320

3420

3520

3620

3720

3820

3920

4020

4120

4220

4320

4420

4520

46

Crew to Phobos

Crew to Mars(24-day stay)

ISS Extension End

Orion First Crewed Flight

SLS Initial Test

Build Up Infrastruc.

Orion Second Crewed Flight

Mars Sim 1Mars Sim 2

Mars Lander Test@Moon

Crew to Mars(1 year)

SEP Demoe.g. ARRM)

Robotic SubscaleEDL Test

EarthCislunar

Mars 38

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Overall Architecture Concept4 SLS Launches

~75 days

Mars

Earth

HEO

HMO

TMI

MOI TEI

Entry

1 2

Deep Space Hab (DSH)

MOI Stage

100 kWeSEP Tug

3

SEP Payload:Phobos Habitat

Phobos

Deep Space Hab + TEI Stage

OrionEUS

4

Crew launch

Phobos BasePre-placement

~200 - 250 days

~200 - 250 days

~300 days

~75 days

~3.5 years

~3.8 years

100 kWeSEP Tug

SEP Payload:TEI Stage +PhobosTransfer Stage(PTS)

Architecture was analyzed for a crew of 4

Deimos

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Short-stay Surface Concept24-Day Surface Stay; Crew of 2; 6 SLS Launches

Architecture was analyzed for a crew of 4, of which 2 land on Mars

Inject to Mars

Loiter in HEO

Mars

Earth

HEO

HMO

TMI

MOI TEI

Entry

1 2

DSHMOI

Stage

Habitat resupply moduleMAV-to-HMO boost stage

Orion EUS

Crew launch

~200 - 250 days

~200 - 250 days

~24 day surface stay

~3.5 years~3.8 years

TEI Stage

LMO

T= -2 days

T= -6 months

T= -4 years

T= -4.5 years

TEI Stage

DSH resupply module

Lander

MAV-to-HMO boost stage

Aerobraketo LMO

~450 days

Aero-capture into HMO

3 4 5

T= -2 years

2-manLander

MAV-to-HMO boost stages

LanderBoost stage

MAV

MAV to LMO

MAV to HMO

Lander

T= -2.5 years

100 kWeSEP Tug

100 kWeSEP Tug

6

EUS

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Cost “Sanity Check”

Aerospace Corporation did the first-look cost assessment

The cost estimating is based on models and analogy - Used model developed for NRC Pathways to Exploration study

- As technical concepts mature, grassroots rather than model-based cost assessments should be performed for budget commitment

Aerospace’s assessment suggests that meeting the Study Team’s self-imposed cost constraint is plausible

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H2MMinimal Architecture

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JPL Architecturewith ISS to 2024

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ISS crew

Phobos Crew

Cis‐Lunar Crew

Mars Long Stay Crew

Lunar Sortie Crew

Mars Short Stay CrewISS to 2024

Current Programs

Support

HSF An

nual Cost

Flat Budget

Phobos Lander2033

Mars LanderShort Stay

2037

Mars Lander Long Stay

2041

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This work was aimed at showing an example (an existence proof)that journeys to Mars using technologies that NASA is currentlypursuing is plausible on a time horizon of interest to stakeholdersand without large spikes in NASA budget.

Takeaway

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HEO Committee Finding

Proposed NASA Human Exploration and Operations Committee Finding

Name of Committee: Human Exploration and Operations CommitteeChair of Committee: Mr. Ken BowersoxDate of Public Deliberation: July 28, 2015 (HEO Advisory Committee)

Short Title of Finding: Outside Participation in Exploration Mission Planning

The HEOMD is leading an effort to build the technical rationale for a sustainable human exploration effort which will allow humans to pioneer space called the Evolvable Mars Campaign. Inclusion of groups outside the core NASA team in the Evolvable Mars Campaign study process helps to build support for the study results, and also allows for a wider set of creative approaches from which to build the final plans for human exploration. The HEO Committee endorses the HEOMD’s current effort to include outside participation in NASA’s planning efforts for the Journey to Mars.

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Transition from ISS to Cis-Lunar Space

A proposed two pronged approach to ensuring that HSFtransitions without a gap between ISS and cis-lunar space

and

research and technology development in LEO continuesseamlessly between ISS end-of-life and

commercially available capabilities

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Transitioning HSF from LEO to Cis-Lunar Space(Earth Dependent to the Proving Ground)

Earth Dependent

‐‐‐

ARM

Knowledge & Capabilities

Long Duration Human Health & HabitationResearch and Demonstrations

First half of the 2020’sProving Ground

Short Duration Habitation & Transportation system validation

Knowledge & Capabilities

SLS/Orion performanceDeep space multi‐body navigationIntegrated crewed/robotic vehicle operations in deep space staging orbitsSystem and crew performance in deep space radiation environmentsAdvanced autonomous proximity operations and rendezvous in deep space and with non‐cooperative objectsAstronaut EVA for sample selection, handling, and containmentValidating Earth return trajectories and emergency return strategies

Second half of the 2020’s

Long duration human health & habitationValidation for Mars transit

Goal: One year crewed mission(s) in cis‐lunar space

Validate crew health and performance countermeasures developed on ISSValidate habitation system and crew performance in deep space radiation environment developed on ISSSimulate Mars transit crew operations –

Limited interaction with MCC based on path finders on ISSLimited/No re‐supplyNo crew exchanges

Develop and validate the operational habitation, life support and environmental monitoring systems that were validated on ISS integrated with other systems (e.g. thermal, power, etc.)

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Implications for the next several years

• Having this goal of a “shake down cruise” (or multiple cruises) near the end of the 2020’s provides an anchor for other HSF activities and possibly broader scientific objectives

Human Spaceflight– Drive SLS/Orion performance and EM mission objectives– Provide the basis for ISS‐to‐PG transition discussions with IP’s– Provides the pull for shorter duration missions – particularl  y ARM– Provides focus for near‐term policy and budgets– Help drive requirements for other areas such as logistics, propulsion, etc. 

Robotic/Science– Lunar robotic exploration– Lunar surface in‐situ demonstration– Cis‐lunar space science objectives

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Commercial and International Partnership

• There are many opportunities for public‐private and international partnerships in achieving the goal of one year duration crewed missions incis‐lunar space

– Habitation and habitation systems– Dissimilar redundancy– Logistical support– Communications– Navigation– Propulsion and re‐fueling systems– Transportation– Other mission or scientific objectives

 

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So What does this mean for ISS

• All the critical research and system demonstrations needed to validate long duration HSF must be completed on ISS…before they are applied in the Proving Ground…– Human research and performance– Habitation systems such as ECLSS, environmental monitoring, crew 

systems, etc.– All the other technologies and systems that need maturation

• Docking, communication protocols, autonomous crew operations, etc.

We are now in the process is determining specifically what transitional objectives we want to accomplish on ISS and what we expect to tranfer to cis‐lunar space– Human research, system performance, operational considerations, etc.

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We are beginning to plan for the transition of HSF out of LEO and into the Proving Ground

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Second Prong: Expand the full breadth of the US economy into LEO

Vision:  Sustained economic activity in LEO enabled by human spaceflight, driven by private and public investments creating value and benefitting Earth through commercial supply and public and private demand

Goals 1.0 LEO commercialization 

enabled by leveraging ISS

2.0 The policy and regulatory 

environment promotes 

commercialization of LEO

3.0  A robust, self‐sustaining, and cost effective supply of US commercial services 

to/in/from LEO accommodates public and 

private demands

4.0 Broad sectors of the economy using LEO for commercial purposes 

• User‐friendly ISS process improvements

• Maximize throughput

• Demonstrate & communicate value proposition of ISS

• Foster “success stories”

• Utilize more commercial acquisition strategies

• Establish interagency working group to address policy and regulatory issues

• Investigate economic cluster potential

• Address barriers such as IP retention, liability, ITAR

• Leverage NASA NEXTStepsBAA studies and follow‐on to enable commercial LEO capabilities

• Enable Earth‐similar laboratory capabilities for ISS that can transition to commercial platforms

• Transition from NASA‐supplied to commercially‐supplied services and capabilities once available

• Establish consortia for potential high‐payoff, market‐enabling microgravity applications with public and private funds to support development (e.g. protein crystallization, exotic fibers, lightweight alloys, 3D tissues)

• Establish commercial LEO utilization university curriculum and programs

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Next HEO NAC

We hope to present a top level draft of the HSF ISS to Proving Ground transition plan and progress towards building the commercial and OGA 

demand for LEO

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Special Topics at Future HEO Committee Meetings

• Future Special Topics:

– International Participation in Future Human Exploration– ISS uses for Exploration development– ISS transition after 2024– Exploration plans after ARM – Launch readiness process for commercial crew– Commercial crew vehicles – contractor briefings

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www.nasa.gov

Speakers Bureau 53


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