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Cloud Download : -Q ;- -... , " NASA-CR-197668 ;' : I "' "l, -; NSTS-08297 - SPACESHUTTLE _,_ooo,,o, 1 J " MISSION REPORT N_ASA _ -J :i (NASA-CR-197668) STS.67 SPACE N96-I1511 SHUTTLE MISSION REPORT .(Lockheed Engineering and Sciences Co.) 49 p Unclas G3116 0068432 May 1995 L SRARYCOPY - | I I i NationalAeronauticsand SpaceAdministration ._ , LyndonB. JohnsonSpaceCenter / "_ _.,_...._. Houston,Texas q • .p • . =j. , NOTE _-_ The STS-67SpaceShuttleMissionReportwaspreparedfrom inputs received fromthe OrbiterProjectas wellas other organizations.Thefollowingpersonnelmaybe contacted should questions arise concerning the technir_l content of this document. KennethL. Brown,JSC Orbiterandsubsystems 713-483-3891 C. A. Snoddy,MSFC MSFCElements(SRB, 205-544-0391 RSRM,SSME,ET, SRSS,andMPS) ElmerL.Taylor,JSC PayloadslExperiments 713-483-1217 G. P. Buoni,JSC DTOsandDSOs 713-483-0639 F.T. Bums;Jr.,JSC FCEandGFE 713-483-1262 .. t' ° DISPLAY 96Ni1511/2 96NI1511"# ISSUE 1 CATEGORY 16 RPT#: NASA-CR-197668 NAS 1.26:197668 NSTS-08297 95/05/01 49 PAGES UNCLASSIFIED DOCUMENT UTTL: STS-67 Space Shuttle mission report _ 7 AUTH: A/FRICKE, ROBERT W., JR. CORP: Lockheed Engineering and Sciences Co., Houston, TX. CSS: (Flight Engineering and Vehicle Management Office.) SAP: Avail: CASI HC A03/MF A01 CIO: UNITED STATES Sponsored by NASA. Johnson Space Center MAJS: /*ENDEAVOUR (ORBITER)/*EXTERNAL TANKS/*POSTMISSION ANALYSIS (SPACECRAFT)/* SPACE SHUTTLE BOOSTERS/*SPACE SHUTTLE MAIN ENGINE/*SPACE SHUTTLE MISSIONS /*SPACE SHUTTLE PAYLOADS/*SPACE TRANSPORTATION SYSTEM MINS: / ASTRO MISSIONS (STS)/ GET AWAY SPECIALS (STS)/ PROPULSION SYSTEM PERFORMANCE/ SPACEBORNE EXPERIMENTS ABA: Derived from text ABS: The STS-67 Space Shuttle Program Mission Report provides the results of the orbiter vehicle performance evaluation during this sixty-eighth flight of the Shuttle Program, the forty-third flight since the return to flight, and the eighth flight of the Orbiter vehicle Endeavour (0V-105). In addition, the report summarizes the payload activities and the performance of the External Tank (ET), Solid Rocket Booster (SRB), Reusable Solid Rocket Motor (RSRM), and the Space Shuttle Main Engines (SSME). The serial ENTER: MORE J ,,I *L"_ _m DISPLAY 96NI1511/2 numbers of the other elements of the flight vehicle were ET-69 for the ET; 2012, 2033, and 2031 for SSME's i, 2, and 3, respectively; and BI-071 for the SRB's. The left-hand RSRMwas designated 36_W043A, and the right-hand RSRM was designated 360L043B. The primary_objective of this flight was to successfully perform the operations of the ultraviolet astronomy (ASTRO-2) payload. Secondary objectives of this flight were to complete the operations of the Protein Crystal Growth - Thermal Enclosure System (PCG-TES), the Protein Crystal Growth - Single Locker Thermal Enclosure System (PCG-STES), the Commercial Materials Dispersion Apparatus ITA Experiments (CMIX), the Shuttle Amateur Radio Experiment-2 (SAREX-2), the Middeck Active Control Experiment (MACE), and two Get-Away Special (GAS) payloads. ENTER: ,dl qL._" NSTS 08297 STS-67 ,i .,.-... : SPACESHUTTLE MISSIONREPORT LESC/FlighEt ngineeringandVehicleManagementOffice Approvedby KennethL. Brown STS-67LeadMissionEvaluationRoomManager W. Camp F--_ Manager,FlightEngineeringandVehicleManagementOffice . _v" Jay H._reene /,,/ Manager,OrbiterProject / _7'BrewsterH. S_haw . Director,SpaceShuttleOperations Preparedby LockheedEngineeringandSciencesCompany for FlightEngineeringandVehicleManagementOffice NATIONALAERONAUTICSANDSPACEADMINISTRATION LYNDONB.JOHNSONSPACECENTER F -. HOUSTON,TEXAS77058 May1995 L • STS-67 Table of Contents F", t Titl.___e Paae ::::::::::::::INTRODUCTION::::::::::::::::::::::::::::::::::::::: 31 PAVLOAOS.............................................. 9 ASTRO-2 LABORATORY.............................. 9 MIDDECK ACTIVE CONTROL EXPERIMENT .............. 9 PROTEIN CRYSTAL GROWTH EXPERIMENTS ............ 10 COMMERCIAL MATERIALS DISPERSIONAPPARATUS INSTRUMENTATION TECHNOLOGY ASSOCIATES EXPERIMENT ..................................... 10 GET-AWAY SPECIAL PAYLOAD I I I I I I I I I I I I I I I I I I I I I i i i 10 SHUTTLE AMATEUR RADIO EXPERIMENT-II .............. 11 VEHICLE PERFORMANCE I I I I I I i I I O e i e • i m • • i -l i e e e i i i i i e I l 12 SOLID ROCKET BOOSTERS ........................... 12 REUSABLE SOLID ROCKET MOTORS ................... 12 EXTERNAL TANK .................................... 13 SPACE SHUTTLE MAIN ENGINES ..................... 14 SHUTTLE RANGE SAFETY SYSTEM..................... 15 ORBITER SUBSYSTEMS PERFORMANCE ................ 15 : Main Propulsion System I I I I I I I I I I I I I I I I I I I I I I I i i i 15 Reaction Control Subsystem ...................... 16 Orbital Maneuverin.qSubsystem.................... 18 Power Reactant Stroraqe and Distribution Subsystem.. 18 Fuel Cell SubsystemI I I I I I I I I I I I I I I I I I I I I I I I I I i i i i 19 Auxiliary Power Unit Subsystem .................... 20 Hydraulics/Water Spray Boiler Subsystem............ 20 Electrical Power Distribution and Control Subsystem .. 21 Environmental Control and Life Support System ...... 21 Aidock Support System .......................... 23 Smoke Detection and Fire Suppression Subsystem.... 23 Avionics and Software Support Systems............. 24 Displays and Controls Subsystems ................. 24 Communications and Trackin.qSubsystems ......... 24 ,OperationalInstrumentationlModular Auxiliary Data System ........................ 25 Structures and Mechanical Subsystems ............. 25 Inte.qratedAerodynamics, Heatinq and Thermal Interfaces................................... 26 STS-67Tableof Contents Titl.___e Paae ThermalControlSubsystem....................... 26 Aerothermodynamics............................. 27 ThermalProtectionSubsystemandWindows......... 27 REMOTEMANIPULATORSYSTEM............................. 29 FLIGHTCREWEQUIPMENTIGOVERNMENTFURNISHED EQUIPMENT................................ 30 CARGOINTEGRATION....................................... 31 DEVELOPMENTTEST OBJECTIVE/DETAILEDSUPPLEMENTARY OBJECTIVE... .............................. 32 DEVELOPMENTTESTOBJECTIVES..................... 32 DETAILEDSUPPLEMENTARYOBJECTIVES............... 34 PHOTOGRAPHYANDTELEVISIONANALYSIS................... 36 LAUNCHPHOTOGRAPHYANDVIDEODATAANALYSIS..... 36 ON-ORBITPHOTOGRAPHYANDVIDEODATAANALYSIS... 36 LANDINGPHOTOGRAPHYANDVIDEODATAANALYSIS.... 36 List of Tables f"_" TABLE I - STS-67SEQUENCEOF EVENTS..................... 37 TABLEII - STS-67ORBITERPROBLEMTRACKINGLIST.......... 39 TABLEIII - STS-67GFE PROBLEMTRACKINGLIST.............. 41 Appendixes A - DOCUMENTSOURCES.................................. A-1 B I ACRONYMSANDABBREVIATIONSl l . i I i i i i i i i i i i i i i i i i l I i BI 1 ii f...... INTRODUCTION t The STS-67SpaceShuttleProgramMissionReportprovidestheresultsoftheOrbiter vehicleperformanceevaluationduringthissixty-eighthflightoftheShuttleProgram, theforty-thirdflightsincethereturntoflight,andtheeighthflightoftheOrbitervehicle Endeavou(OVr -105). Inaddition,thereportsummarizesthepayloadactivitiesandthe performanceoftheExternalTank(ET),SolidRocketBooster(SRB),ReusableSolid RocketMotor(RSRM),andtheSpaceShuttlemainengines(SSME). The serialnumbersoftheotherelementsof theflightvehiclewereET-69fortheET; 2012,2033 and2031forSSMEs1,2, and3, respectively;andBI-071fortheSRBs. The left-handRSRMwasdesignated360W043A,andtheright-handRSRMwas designated360L043B. The primaryobjectiveof thisflightwastosuccessfullyperformtheoperationsofthe UltravioletAstronomy(ASTRO-2)payload.Secondaryobjectivesofthisflightwereto completetheoperationsoftheProteinCrystalGrowth- ThermalEnclosureSystem (PCG-TES),theProteinCrystalGrowth- SingleLockerThermalEnclosureSystem (PCG-STES),theCommercialMaterialsDispersionApparatusITAExperiments (CMIX),theShuttleAmateurRadioExperiment-II(SAREX-II),theMiddeckActive ControlExperiment(MACE),andtwoGet-AwaySpecial(GAS)payloads. The STS-67missionwasplannedasa 16-daymissionplustwo.contingencydays,one forweatheravoidanceandoneforcontingencyoperations.Thesequenceofeventsfor theSTS-67missionisshowninTableI, theOrbiterProjectProblemTrackingListis showninTableII, andtheGovernmentFurnishedEquipment(GFE)ProblemTracking ListisshowninTableII1. Inaddition,anyIntegrationin-flightanomaliesarereferenced intheapplicablesectionsofthereport.AppendixA liststhesourcesofdata,both formalandinformal,thatareusedinthepreparationofthisreport.AppendixB providesthedefinitionof acronymsandabbreviationsfoundinthereport. Alltimesare listedinGreenwichmeantime(G.m.t.)aswellasmissionelapsedtime(MET). The seven-personcrewforSTS-67consistedof StephenS. Oswald,Civilian, CommanderWilliam; G. Gregory,Lt.Col.,USAirForce,Pilot;JohnM. Grunsfeld, Ph. D, Civilian,MissionSpecialist1;WendyB. LawrenceUSN,, CDR(Select),flight engineerandMissionSpecialist2;TamaraE. Jernigan,Ph.D.,Civilian,Payload CommanderandMissionSpecialist3; SamuelT. Durrance,Ph.D.,Civilian,Payload Specialist1;andRonaldParise,Ph.D.,Civilian,PayloadSpecialist2. STS-67wasthe thirdspaceflightfortheCommandeandr MissionSpecialist3, thesecondspaceflight• forbothpayloadspecialists,andthefirstspaceflightforthePilot,MissionSpecialist1, andMissionSpecialist2. .L The STS-67SpaceShuttleProgramMissionReportfulfillstheSpaceShuttleProgram requirementas documentedinJSC07700,VolumeVIII,AppendixE. The requirement F'-"._ thatisstatedinthatdocumentisthateachmajororganizationalelementsupportingthe Programwillreporttheresultsoftheirhardware(andsoftware)evaluationandmission performanceplus, identifyallrelatedin-flightanomalies. The MarshallSpaceFlightCenter(MSFC)STS-67FlightEvaluationReportscontain
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