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EIGHTH ANNUAL
AIAA/UTAH STATE UNIVERSITY
CONFERENCEon
SMALL SATELLITES
Dr. Frank J. ReddGeneral Chairperson
R. Gilbert MooreProgram Chairperson
Janell H. LarsonConference Services
Gwenaley Redd-HardyConference Coordinator
UTAH STATE UNIVERSITYLOGAN, UTAH 84322
August 29 - September 1, 1994
TECHNICAL SESSION IHARDWARE IN SPACE
Tuesday, August 30, 10:45 a.m. - 12:15 p.m.
Chairperson: Mr. Jim French, JRF Engineering Services
MARS PATHFINDER FLIGHT SYSTEM DESIGN AND IMPLEMENTATION * *B. K. Muirhead, R. Manning, and C. Cleven - Jet Propulsion Laboratory
THE TWO UK 'SPACE TECHNOLOGY RESEARCH VEHICLES': FIRSTIN-ORBIT RESULTS * *
K. A. Ryden, N. Wells, A. Christmas, and N. Wallace - DefenceResearch Agency
MINIATURE SENSOR TECHNOLOGY INTEGRATION (MSTI) FLIGHT TESTRESULTS
D. L. Erickson - SPARTA, Inc.; J. R. Feig, E. C. Grigsby - USAFPhillips Laboratory; and J. A. Carlson - Loral EOS
ONE YEAR IN SPACE: RESULTS FROM PoSAT-1 * *M. Meerman, M. Sweeting - Centre for Satellite Engineering Research,University of Surrey, U.K.; and M. Leitmann - LAER/INETI, Portugal
BREM-SAT - FIRST FLIGHT RESULTSH. Konigsmann, H. W. Oelze, and H. J. Rath - University of Bremen,Germany
RECENT LIGHT SATELLITE MISSIONS AND ACCOMPLISHMENTS IN THEDoD SPACE TEST PROGRAM * *
D. England, T. Hagler - ANSER; and E. Witte - AeroSpace Corporation
* * ABSTRACT PRINTED - PAPER NOT RECEIVED IN TIME FOR PUBLICATION
TECHNICAL SESSION IISMALLER, CHEAPER, FASTER
Tuesday, August 30, 1:30 p.m. - 3:00 p.m.
person: Melanie Horn Dynes, Aero Astro
MANAGING A "BETTER, FASTER, CHEAPER" LIGHTSAT PROGRAM * *D. V. Shuckstes - TRW Space & Electronics Group
STANDARDIZATION OF THE LAUNCH VEHICLE INTERFACE FOR SMALLPAYLOADS * *
D. O'Connell, D. Miller, P. Fleming, and F. Little - CTA LaunchServices
A NEW APPROACH TO FLIGHT EQUIPMENT: CLEMENTINE AND MSTIWORK AT JPL
K. A. Hicks and J. W. Wall - Jet Propulsion Laboratory
CLEMENTINE: NEW DIRECTIONS AND PERSPECTIVES FOR ONE-OF-A-KINDSPACECRAFT MISSIONS * *
P. A. Regeon - Naval Research Laboratory; R. J. Chapman - Praxis,Inc.; and R. Baugh - Barrios Technology, Inc.
A COST MODEL FOR A UNIVERSITY SATELLITE PROGRAME. I. Reeves - U.S. Air Force Academy
DEPENDABILITY DESIGN FOR THE PLUTO FLYBY MISSIONS. B. Johnson, L. P. Cooper, and D. D. Uhrich - University ofCincinnati Space Engineering Research Center
ABSTRACT PRINTED - PAPER NOT RECEIVED IN TIME FOR PUBLICATION
TECHNICAL SESSION IVNEW MISSIONS I
Wednesday, August 3 1 , 9:15 a.m. - 10:45 p.m.
Chairperson: Mr. Rex Ridenoure, Jet Propulsion Laboratory
NEAR EARTH ASTEROID RETURNED SAMPLE MISSION (NEARS)A. F. Cheng and S. R. Vernon - The Johns Hopkins University AppliedPhysics Laboratory
LESSONS LEARNED FROM CLEMENTINE ON THE WAY TO PLUTOJ. Carraway, P. Henry, M. Herman, G. Kissel, H. Price, R. Staehle, andM. Underwood - Jet Propulsion Laboratory
SCIENCECRAFT * *P. M. Beauchamp, R. H. Brown, R. W. Capps, D. H. Rodgers, J .Sercel, G. Vane - Jet Propulsion Laboratory; L. A. Soderblom - UnitedStates Geological Survey; and R. V. Yelle - Lunar and PlanetaryLaboratory, University of Arizona
THE SATELLITE QUICK RESEARCH TESTBED (SQUIRT) PROGRAMC. A. Kitts and R. J. Twiggs - Satellite Systems DevelopmentLaboratory, Stanford University
THE ROCSAT-1 SAPCECRAFT * *C. F. Lillie, R. E. Sharpies - TRW; and K. Yong - National SpaceProgram Office, Republic of China, Taiwan
SKIPPER: A SMALL SATELLITE FOR UPPER ATMOSPHERIC STUDIESL. C. Howlett - Space Dynamics Laboratory/Utah State University;G. Malyshev - Moscow Aviation Institute; and D. Levin - Institute forDefense Analyses
ABSTRACT PRINTED - PAPER NOT RECEIVED IN TIME FOR PUBLICATION
TECHNICAL SESSION VUNIVERSITY STUDENT SESSION
Wednesday, August 3 1 , 11:00 a.m. - 12:45 p.m.
Chairperson: Jayne Schnaars, Rockwell International CorporationRobert H. Muerer, Orbital Sciences Corporation
PRELIMINARY DESIGN OF ASUSat 1J. Rademacher - Arizona State University
A MICROPARTICLE RECOGNITION EXPERIMENT FOR NEAR-EARTH SPACEON BOARD THE SATELLITE ASUSat 1
C. Hewett - Arizona State University
DESIGN OF THE ISAT-1 SATELLITE THERMAL CONTROL SYSTEMJ. Clay - University of Iowa
• MINIATURIZATION METHODS FOR DEEP SPACE MICROSPACECRAFTL. Muller - Massachusetts Institute of Technology
THE DESIGN AND CONSTRUCTION OF THE STANFORD AUDIO PHONICPHOTOGRAPHIC INFRARED EXPERIMENT (SAPPHIRE) SATELLITE
C. Kitts and B. Kim - Stanford University
ISAT-1 COMMUNICATION SYSTEMM. Lu and K. Chen - Iowa State University
EXPERIMENTAL TESTS OF VARIOUS "BANG-BANG" CONTROLLERS ONTHE SMALL SATELLITE ATTITUDE CONTROL SIMULATOR
S. Kuntanapreeda, J. Jones, and J. Crookston - Utah State University
SolSTUS - SOLAR SOURCE THERMAL UPPER STAGE *D. Jones - Utah State University
* ALTERNATE - PRESENTATION IN THE POSTER SESSION
TECHNICAL SESSION IIIOPERATIONS AND SOFTWARE
Tuesday, August 30, 3:30 p.m. - 5:00 p.m.
Chairperson: Shaun Anderson, Orbital Sciences Corporation
DEMONSTRATION OF ON-BOARD MANEUVER PLANNING USINGAUTONOMOUS S/W ARCHITECTURES * *
A. Ahmed, D. Eldred, and A. S. Aljabri - Jet Propulsion Laboratory
THE ZIPSIM SERIES OF HIGH PERFORMANCE, HIGH FIDELITY SPACECRAFTSIMULATORS
W. K. Reinholtz and W. J. Robison, III - Jet Propulsion Laboratory
MSTI-3 SPACECRAFT ATTITUDE CONTROL SOFTWARE DEVELOPMENTUSING AUTOMATIC CODE GENERATION * *
F. Tubb, R. McEwen, J. Farazian, and A. Waddell - Integrated SystemsInc.
MSTI-3 SCIENCE OBJECTIVESW. Jeffrey - Institute for Defense Analyses; J. Fraser - PhotonResearch Associates; and G. Schneider - Ballistic Missile DefenseOrganization
THE IN-ORBIT OPERATION OF FOUR MICROSAT SPACECRAFT-FOURYEARS LATER
R. J. Diersing - Texas A&M University-Kingsville
• MSTI COMMANDER-IN-THE-FIELD "BATTLEFIELD" PAYLOAD COMMANDDEMONSTRATION * *
T. C. Probert - ANSER; and D. R. Lockwood - Storm Integration, Inc.
ABSTRACT PRINTED - PAPER NOT RECEIVED IN TIME FOR PUBLICATION
TECHNICAL SESSION VISUBSYSTEMS I
Wednesday, August 3 1 , 2:00 p.m. - 3:30 p.m.
Chairperson: John Patton, Idaho National Engineering Laboratory
THE CLEMENTINE ATTITUDE DETERMINATION AND CONTROL SYSTEMP. DeLaHunt, S. Gates, M. Levenson - U.S. Naval ResearchLaboratory; and G. Creamer - Swales & Associates
DESIGN AND FABRICATION OF A LOW-COST COMPOSITE SPACEFRAMESPACECRAFT STRUCTURE
J. Scherrer, G. Dirks - Southwest Research Institute; A. Campbell, andR. Sanderson - Texas Composite, Inc.
• RELIABLE APPLICATION OF PLASTIC ENCAPSULATED MICROCIRCUITSFOR SMALL SATELLITES
W. A. Ash III and E. J . Hoffman - The Johns Hopkins UniversityApplied Physics Laboratory
A LOW COST TAILORABLE POWER SOURCE FOR MICROSATELLITES * *P. A. Dillard - Boeing Defense & Space Group
THE CLEMENTINE NICKEL HYDROGEN COMMON PRESSURE VESSELBATTERY
J. C. Garner - U.S. Naval Research Laboratory
TOWARDS REDUCED NICKEL-CADMIUM BATTERY COST FOR MICROSATELLITES
V. Cavenel and D. Duquesne - SAFT
ABSTRACT PRINTED - PAPER NOT RECEIVED IN TIME FOR PUBLICATION
TECHNICAL SESSION VIIINEW MISSIONS II
Thursday, September 1, 8:30 a.m. - 10:00 a.m.
Chairperson: Helene Schember, Jet Propulsion Laboratory
DEVELOPMENT OF THE 0RSTED SATELLITE PROJECTW. R. Baron, M. Houghton-Larsen, and P. L. Thomsen - ComputerResources International, Denmark
A STUDENT SPACECRAFT FOR IN-ORBIT TEST OF NASA TRACKINGPROGRAMS * *
J. G. Smith, S. E. Johnson, R. C. Clauss, and R. W. Ridenoure - JetPropulsion Laboratory
CONCEPTUAL DESIGN OF A HIGH-RESOLUTION, LOW COSTTOPOGRAPHIC MAPPING MISSION * *
S. Jolly, W. McClintock, D. Lawrence, R. Su, A.F. H. Goetz, D.Mackison - University of Colorado, Boulder; and D. Baker - DABEngineering, Inc.
STATUS OF THE THIRD MINIATURE SENSOR TECHNOLOGY INTEGRATIONSATELLITE MISSION * *
D. Barnhart, R. Hurtz - Phillips Laboratory; J. McClelland - SpectrumAstro; M. Cellarius - Sparta; and A. Meyers - SAIC
TOMS-EP SPACECRAFTA. Azarbarzin - NASA/GSFC; B. Dobrotin and A. Fleming - TRW
MSTI-3 DUAL-USE APPLICATIONS * *J. Hood - ANSER; and W. Jeffrey - Institute for Defense Analyses
* * ABSTRACT PRINTED - PAPER NOT RECEIVED IN TIME FOR PUBLICATION
TECHNICAL SESSION IXINSTRUMENTATION AND SENSORS
Thursday, September 1, 10:30 a.m. - 12:00 a.m.
Chairperson: Dr. Allan Steed, Space Dynamics Laboratory
• DESIGN AND DEVELOPMENT OF THE CLEMENTINE SPACECRAFT SENSORBENCH * *
J. Kim, S. Koss, R. Mader, and D. Spencer - Naval ResearchLaboratory
SMALL EARTH IMAGING SPECTROMETER * *G. Vane, J. J. Simmonds, D. H. Rodgers, M. Chrisp, G. Chen, G.Fraschetti, C. Bruce, R. O. Green, D. Johnson, C. Mahoney, J. Neslte,W. Petrick - Jet Propulsion Laboratory; A. F. H. Goetz - University ofColorado, Boulder; and C. 0. Davis - U.S. Naval Research Laboratory
PLUTO INTEGRATED CAMERA-SPECTROMETER (PICS): A LOW MASS,LOW POWER INSTRUMENT FOR PLANETARY EXPLORATION * *
P. M. Beauchamp, R. H. Brown, D. H. Rodgers, M. P. Chrisp, G. Chen,G. A. Fraschetti T. N. Krabach, S. W. Petrick - Jet PropulsionLaboratory; L. A. Soderblom - USGS; R. V. Yelle - University ofArizona; R. T. Benoit, M. E. Curcio, R. R. Glasheen, T. W. Tucker, andD. Wang - SSG, Inc.
MSTI-3 BACKGROUND DATA-COLLECTION EXPERIMENTW. Jeffrey, P. Albright - Institute for Defense Analyses; A. Ratkowski- Phillips Laboratory, PL/GPO; and J. Hood - Analytic Service, Inc.
SPACECRAFT ENVIRONMENT AND SYSTEMS MONITORINGINSTRUMENTATION FOR SMALL SATELLITES * *
P. B. Joshi, et al. - Physical Sciences, Inc.; and D. Brinza - JetPropulsion Laboratory
CHEMICAL AND ELECTRIC PROPULSION OPTIONS FOR SMALL SATELLITESR. M. Myers, S. R. Oleson, F. M. Curran, and S. J . Schneider - NASALewis Research Center
* * ABSTRACT PRINTED - PAPER NOT RECEIVED IN TIME FOR PUBLICATION
TECHNICAL SESSION VIITESTING, VERIFICATION, & VALIDATION
Wednesday, August 3 1 , 4:00 p.m. - 5:30 p.m.
Chairperson: Dr. Jim Romero, University of New Mexico
SPIN BALANCE PROCESSING OF THE CLEMENTINE SPACECRAFTP. V. Dizon - Barrios Technology, Inc.
MSTI-III CALIBRATION AND CHARACTERIZATIONR. W. Gobel - ANSER Corporation; and A. Ratkowski - PhillipsLaboratory/GPO
AN INNOVATIVE APPROACH TO DETERMINE THE ALIGNMENT OF THESTAR CAMERA SYSTEM FOR THE CLEMENTINE SPACECRAFT
M. R. Corson, J. H. Resnick, C. J. Rollins - Research SupportInstruments; P. G. DeLaHunt, P. R. Lynn, Jr. - U.S. Naval ResearchLaboratory; and M. J. Pilecki - Allied Signal Corporation
THERMAL DESIGN OF THE FAST-ON-ORBIT RECORDING OF TRANSIENTEVENTS (FORTE) SATELLITE * *
R. L. Akau, V. L. Behr - Sandia National Laboratories; and R. Whitaker- Los Alamos National Laboratory
• VIBRO-ACOUSTIC TESTING OF THE CLEMENTINE SPACECRAFT * *J. M. Haughton - Kinetic Research Corporation; J. Layher, R. Haynes,and J. Hauser - Naval Research Academy
• ON ORBIT JITTER SIMULATION TESTING OF THE CLEMENTINESPACECRAFT * *
J. M. Haughton - Kinetic Research Corporation; and D. Spencer -Naval Research Laboratory
* * ABSTRACT PRINTED - PAPER NOT RECEIVED IN TIME FOR PUBLICATION
TECHNICAL SESSION XCOMMUNICATIONS
Thursday, September 1, 1:30 p.m. - 2:45 p.m.
Chairperson: Dr. Kermit W. Reister, Weber State University
CCSDS SPACECRAFT UPLINK PROTOCOL IN A SPACE-QUALIFIED ASICS. H. Wood, G. S. Bolotin, and J. A. Donaldson - Jet PropulsionLaboratory
• LOSSLESS COMPRESSION AND RATE CONTROL FOR THE GALILEO NIMSINSTRUMENT * *
R. F. Rice and R. Mehlman - Jet Propulsion Laboratory
GLOBAL RATE ALLOCATION AND CONTROLR. F. Rice - Jet Propulsion Laboratory
SMALL DEEP SPACE MISSION TELECOMMUNICATIONSG. K. Noreen, A. L. Riley, and V. M. Pollmeier - Jet PropulsionLaboratory
THE FORTE' RECEIVER AND SUB-BAND TIRGGERING UNITD. C. Enemark and M. E. Shipley - Los Alamos National Laboratory
* * ABSTRACT PRINTED - PAPER NOT RECEIVED IN TIME FOR PUBLICATION
TECHNICAL SESSION XISUBSYSTEMS II
Thursday, September 1, 3:00 p.m. - 4:30 p.m.
Chairperson: Sven Grahn, Swedish Space Corporation
• THE NEXT-GENERATION SC-7 RISC SPACEFLIGHT COMPUTERD. J. Shirley and M. K. McLelland - Southwest Research Institute
IN ORBIT ATTITUDE DETERMINATION, CONTROL AND STABILIZATIONPERFORMANCE OF THE STRV 1A AND 1B MICROSATELLITES FROM THEUK DEFENCE RESEARCH AGENCY * *
M.E. Huddleston, N. Wells, K. A. Ryden and B. Cocking - DefenceResearch Agency
THE MARS PATHFINDER ATTITUDE AND INFORMATION MANAGEMENTSYSTEM * *
D. H. Lehman and D. Woerner - Jet Propulsion Laboratory
RADIATION HARDENED MICROPROCESSOR FOR SMALL SATELLITES,PAYLOADS AND INSTRUMENTS * *
R. Shah - Harris Corporation
DEVELOPMENT OF AN ALL-COMPOSITE SPACECRAFT BUS FOR SMALLSATELLITE PROGRAMS
T. C. Thompson, C. Grastataro, B. Smith - Los Alamos NationalLaboratory; G. C. Krumweide and G. A. Tremblay - Composite Optics,Inc.
• ADVANCED TECHNOLOGY OSCILLATOR FOR THE PLUTO FLYBY MISSIONJ. R. Norton - The Johns Hopkins University Applied PhysicsLaboratory
• FASat-Alfa: STATUS REPORT OF THE FIRST CHILEAN SATELLITE * *F. F. Mujica - Chilean Air Force
* * ABSTRACT PRINTED - PAPER NOT RECEIVED IN TIME FOR PUBLICATION
ABSTRACTS ACCEPTED FOR POSTER SESSION
ALIGNMENT, CALIBRATION, AND INTEGRATION OF THE CLEMENTINEIMAGING CAMERAS
C. Rollins, M. Corson, J. Resnick, J. Ivory - Research SupportInstruments; I. Lewis - Lawrence Livermore National Laboratory; andW. Collins - U.S. Naval Research Laboratory
COMMERCIAL REMOTE-SENSING PAYLOADS FOR SMALL SATELLITESR. Green, M. Herring, and J. Simmonds - Jet Propulsion Laboratory
THE TELEDESIC SPACE SEGMENT ARCHITECTURE, TECHNOLOGIES ANDDESIGN FEATURES
J. R. Stuart - Teledesic Corporation
MECHANISNS SUBSYSTEM FOR THE CLEMENTINE SPACECRAFTB. Purdy and M. Hurley - Naval Research Laboratory
ORBITAL ANALYSIS OF A SUN SYNCHRONOUS SMALL SATELLITE *E. I. Reeves and D. D. Garber - U.S. Air Force Academy
THE ORBITING OZONE AND AEROSOL MONITOR (OOAM) * *R. Bevilacqua, J. Hornstein, W. Glaccum - Naval Research Laboratory;M. Tollin, S. Thompson - TRW Space & Electronics Group; and MikeGangl, et al. - Research Support Instruments, Inc.
THE FAISAT STORE AND FORWARD SATELLITE AND ASSOCIATEDSYSTEMS
N. Modanlo and R. Megill - Final Analysis Incorporated
BEYOND SEDSAT: DESIGNING A MICROSATELLITE FOR ANINTERPLANETARY SCIENCE MISSION
D. R. Wingo and N. Myers - University of Alabama Huntsville
QUICKSAT: A LOW COST, QUICK TURN-AROUND SPACECRAFT BUSTAILORED TO SPECIFIC INSTRUMENT AND MISSION REQUIREMENTS
W. Lockhart, J. Scherrer, and G. Dirks - Southwest Research Institute
CLOSED-LOOP ATTITUDE CONTROL FOR A SMALL SATELLITEA. Schneider and M. Tseng - University of California at San Diego
CLEMENTINE: A FAST TRACT APPROACH TO SPACECRAFT MECHANICALASSEMBLY. INTEGRATION & TEST. AND PROCESSING
W. C. Raynor and P. R. Lynn - Naval Research Laboratory
• OPTIMIZATION OF THE TWO-IMPULSE RENDEZVOUS MANEUVER OF TWOSPACECRAFT IN CIRCULAR ORBIT
G. Raikunov and V. Loukiachtchenko
• AN ANALYSIS OF THE OPTIMAL1TY OF THE TWO-IMPULSE RENDEZVOUSMANEUVERS OF TWO SPACECRAFT IN CIRCULAR ORBIT
G. Raikunov and V. Loukiachtchenko
• A HIGH CAPABILITY, LOW COST UNIVERSITY SATELLITE FORASTROPHYSICAL RESEARCH *
K. Levenson - University of New Hampshire; and K. Reister - WeberState University
• THE ATTITUDE CONTROL HARDWARE AND ALGORITHMS FOR FINEPOINTING OF SUNSAT DURING IMAGING
H. Steyn - University of Stellenbosch, South Africa
• PRECISION ANALOG SUN SENSOR (PASS): A High Accuracy, Light Weight,Low Cost Sun Sensor for the SmallSat Community
C. Zaffanella - EDO Corporation, Barnes Engineering Division
• STATIONARY PLASMA THRUSTER STATUS AND THE IMPACT OF SPTAPPLICATION ON SMALL SATELLITE MISSIONS
C. W. Clauss - Atlantic Research Corporation
• SUMMARY OF CURRENT SOLAR CELL TECHNOLOGIES FOR SPACE ARRAYDESIGN
B. Reed - Satellite Power Corporation
• THE LOW-COST HYBRID PROPULSION SYSTEM RESEARCH PROGRAMMEAT THE UNIVERSITY OF SURREY
J. J. Sellers, M. Meerman, M. Sweeting - Centre for SatelliteEngineering Research, University of Surrey, U.K.
• THE CONESTOGA 1620 FIRST FLIGHTB. Saavedra - EER Systems Corporation
* PAPER PRINTED
* * ABSTRACT PRINTED - PAPER NOT RECEIVED IN TIME FOR PUBLICATION