13Th Space Simulation Conference

13Th Space Simulation Conference

NASA Conference Publication 2340 13th Space Simulation Conference The Payload- Testing for Success H Proceedings of a symposium held at Sheraton Twin Towers, Orlando, Florida October 8-11, 1984 H r _ '_:_!i_!:_ii__ =,, = _. U L: ¸ NASA Conference Publication 2340 13th Space Simulation Conference The Payload- Testing for Success Sponsored by National Aeronautics and Space Administration Institute of Environmental Sciences The American Institute for Aeronautics and Astronautics The American Society for Testing and Materials Proceedings of a symposium held at Sheraton Twin Towers, Orlando, Florida October 8-11, 1984 IW_,A National Aeronautics and Space Administration Scientific and Technical Information Branch 1984 P REFAC E The Thirteenth Space Simulation Conference, held at the Sheraton Twin Towers, Orlando, Florida, October 8-11, 1984 was sponsored by the Institute of Environmental Sciences and supported by the National Aeronautics and Space Administration, the American Institute of Aeronautics and Astronautics, and the American Society for Testing and Materials. These conferences have brought together engineers and scientists of diverse disciplines with the common interests of space simulation, its applications and solutions of complex problems that are encountered. This conference was favored with a wide variety of papers concerning facilities, testing and contamination control. Our featured speaker was Francis J. Logan, Deputy Project Manager, Solar Maximum Repair Mission, who spoke of the problems and successes of retrieving and repairing an orbiting spacecraft utilizing the Shuttle. This endeavor was a historic first for the space program. The meeting was concluded with a trip to the Kennedy Space Center to see the Shuttle complex and other points of interest. I wish to acknowledge the splendid effort of the many people who made this meeting successful. Robert P. Parrish, Jr., Martin Marietta Corp., Technical Program Chairman and his committee gave us a well rounded, informative program; Joseph L. Stecher, NASA GSFC, as Publications Chairman assembled these proceedings; John D. Campbell, Perkin Elmer Corp., was extremely helpful in his capacity as the IES Meeting Manager; and Betty Peterson, IES Executive Director, and Janet A. Ehman, IES Deputy Executive Director, did their usual excellent efforts in all administrative areas. R. T. Hollingsworth General Chairman 111 COMMITTEES FOR 13TH SPACE SIMULATION CONFERENCE MEETING MANAGEMENT COMMITTEE General Chairman: Russell T. Hollingsworth, NASA Goddard Space Flight Center Technical Program: Robert P. Parrish, Jr., Martin Marietta Corporation IES Meeting Manager: John D. Campbell, Perkin-Elmer Corporation Publication Chairman Joseph L. Stecher III, NASA Goddard Space Flight Center Facilities Chairman: James E. Easley, Micro Filtrations Inc. IES Deputy Executive Director: Janet A. Ehmann, Institute of Environmental Sciences IES Executive Director: Betty Peterson, Institute of Environmental Sciences TECHNICAL PROGRAM COMMITTEE Ernest Oddo, The Aerospace Corporation Steven W. Liu, TRW Ward F. Petrie, Perkin-Elmer Corporation Raymond Kruger, NASA Goddard Space Flight Center John Harrell, Jet Propulsion Laboratory David G. Billingsley, Lyndon B. Johnson Space Center Raymond Rempt, Martin Marietta Aerospace Eugene N. Borson, The Aerospace Corporation JOINT POLICY COMMITTEE IES John D. Campbell, Perkin-Elmer Corp. George Frankel, Grumman Aerospace ASTM Eugene N. Borson, Aerospace Corp. Charles H. Duncan, NASA-GSFC AIAA David G. Billingsley, NASA Johnson Space Center Albert R. Lunde, The Boeing Company CONTENTS Section Page SESSIONI: FACILITIES Chairmen:RaymondRempt,Martin MariettaAerospace Albert R. Lunde,BoeingAerospace DEVELOPMENTOFA THERMAL ENVIRONMENTSIMULATOR FOR LARGETESTARTICLESIN A VACUUM ..................................................... Hal B. Storrs,Martin MariettaAerospace INNOVATIVE METHOD FORTHE THERMAL CYCLING OF LARGESPACECRAFTSYSTEMS............................................................... C. H. SteimerandA. D. Hale,TRW SPACESIMULATION TESTINGOFTHE EARTH RADIATION BUDGETSATELLITE ............................................................................... 21 EdwardMagetteandDerrinSmith, Ball AerospaceSystemsDivision MAIN CHARACTERISTICSOF THE LARGE SPACESIMULATOR AT ESA/ESTEC....................................................................................... 30 P. W. Brinkman,ESA/ESTEC SESSIONII: FACILITIES Chairmen: John Harrell, Jet Propulsion Laboratory Don Ridley, TRW SIMULTANEOUS THERMAL VACUUM TESTING OF GPS DRIVE FOR NAV STAR .............................................................................................. 52 T. G. Brown, Ball Aerospace Systems Division THE SCEPTRE FACILITY: IMPROVED SIMULATION OF THE SPACE ENVIRONMENT THROUGH THE APPLICATION OF ADVANCED TECHNOLOGY ........................................................................................ 57 J. D. Ruley, The University of Dayton STANDARDIZATION AND SOFTWARE CONVERSION OF (ROM) ESTIMATING .......................................................................................... 72 G. Roat, Martin Marietta Aerospace FATIGUE INDUCED FAILURES IN ALUMINUM LN 2 SHROUDS OF 39 FOOT VACUUM CHAMBER ...................................................................... 77 Arthur Edwards, Ford Aerospace and Communications Corporation vii Section Page SESSIONIII: SPECIALTOPICS Chairmen:EugeneBorson,TheAerospaceCorporation George F. Wright, Sandia National Laboratories SPACE SHUTTLE REACTION CONTROL SYSTEM (RCS) PROPELLANT TANK MASKED SCREEN TEST .................................................................. 101 J. B. Henderson, NASA Johnson Space Center GROUND TEST CHALLENGES IN THE DEVELOPMENT OF THE SPACE SHUTTLE ORBITER AUXILIARY POWER UNIT .......................................... 111 Norman H. Chaffee, Renee' J. Lance, and Dwayne P. Weary, NASA Johnson Space Center PANEL: SIMULATION OF UPPER ATMOSPHERE OXYGEN SATELLITE EXPOSURE TO ATOMIC OXYGEN IN LOW EARTH ORBIT ............ 133 Daniel R. Peplinski, Graham S. Arnold, and Eugene N. Borson, The Aerospace Corporation HYPERVELOCITY SUPERSONIC NOZZLE BEAM SOURCE OF ATOMIC OXYGEN ................................................................................................ 146 A. Freedman, W. Unkel, J. Silver, and C. Kolb, Aerodyne Research Inc. A FACILITY FOR INVESTIGATING INTERACTIONS OF ENERGETIC ATOMIC OXYGEN WITH SOLIDS ........................................................................... 150 Graham S. Arnold and Daniel R. Peplinski, The Aerospace Corporation AN ATOMIC OXYGEN FACILITY FOR STUDYING POLYMER MATERIALS FOR SPACECRAFT APPLICATION ............................................................ 169 R. C. Tennyson, J. B. French, L. J. Kok, and J. Kleiman, University of Toronto Institute for Aerospace Studies. D. G. Zimcik, Communications Research Centre [Canada] A LOW EARTH ORBIT MOLECULAR BEAM SPACE SIMULATION FACILITY ............................................................................................... 193 Jon B. Cross, Los Alamos National Laboratory THE ENERGY DEPENDENCE AND SURFACE MORPHOLOGY OF KAPTON DEGRADATION UNDER ATOMIC OXYGEN BOMBARDMENT ...................... 205 Dale C. Ferguson, Lewis Research Center ATOMIC BEAM SYSTEM FOR LABORATORY SIMULATION OF UPPER ATMOSPHERIC OXYGEN ATOMIC IMPACT ON STS SURFACES ................... 222 P. Mahadevan, The Aerospace Corporation °°. VIII Section Page SESSION IV: MEASUREMENTS AND TECHNIQUES Chairmen: Steve Liu, TRW Emile S. J. Wang, McDonnell Aircraft Co. 228 LEAK DETECTOR FOR SPACECRAFT TESTING WITH HIGH ACCURACY ........ G. S/inger, and A. K. Franz, European Space Agency/ESTEC 248 DESIGN OF ORBITAL HEATING SIMULATOR USING IR TECHNIQUES ............ M. Donato and A. Harris, Spar Aerospace Ltd; B. Muir, David Florida Laboratories 265 TAPE HEATING METHOD FOR SPACE SIMULATION TESTING ....................... R. Clifford and H. Presley, TRW SESSION V: SOLAR MAX MISSION Chairmen: David G. Billingsley, NASA Johnson Space Center Richard Hartenbaum, RCA THE ROLE OF THE SHUTTLE ENGINEERING SIMULATOR IN THE SOLAR 276 MAX RESCUE MISSION ...................................................................... _..... H. St. John, NASA Johnson Space Center, Bernd Strassner, Lockheed Engineering and Management Services Co., Inc. MANNED MANEUVERING UNIT SIMULATION ON THE SPACE OPERATIONS 295 SIMULATOR ........................................................................................... C. Hartley, L. Ray, and D. Cwynar, Martin Marietta Aerospace SESSION VI: MEASUREMENTS AND TECHNIQUES Chairmen: Ward Petrie and A. Westfall, Perkin-Elmer Corporation DISTORTION MEASUREMENT OF ANTENNAS UNDER SPACE SIMULATION CONDITIONS WITH HIGH ACCURACY AND HIGH RESOLUTION BY 309 MEANS OF HOLOGRAPHY ....................................................................... Dr. Holm Frey, IABG, West Germany 320 VIBRATION ISOLATION SYSTEM FOR TESTING IN A VACUUM ...................... J. Dankowski, Barry Controls PREDICTIVE THERMAL-VACUUM MODELING BY VARIABLE 340 COEFFICIENTS ....................................................................................... J. Chuvala, Perkin-Elmer ix Section Page SESSIONVII: CONTAMINATION AND MATERIALS Chairmen:RaymondKrugerandJackTriolo, NASA GoddardSpaceFlight Center IMPROVEDMATERIALS CHARACTERIZATION FOR SPACECRAFT APPLICATIONS ...................................................................................... 341 Lt. R. Cull, USAF, Wright-Patterson AFB, OH. PREPARATION AND CLEANLINESS VERIFICATION OF A SPACE SIMULATION CHAMBER FOR

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