msfc skylab orbital workshop, volume 3

8/8/2019 MSFC Skylab Orbital Workshop, Volume 3

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; NASA TECHNICAL May 1974

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" L;,-4/ L_,MSFCSKYLABORBITALWORKSHOP _- ',,,.Vol. III ., =.. .._ _Skylab Program Office ! ' "" _NASA ' "_ _

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GeorgeC. Marshall Space Flight CenterMarshall SpaceFlight Center, Alabama

(i _$I-TB- X- 6q813-ol-3) BSFC SK_L_B !/7_-28330_BI_&L iiO_SBOP, VOLUB_. 3 (llAS_) _,_9 I_BC $13,00 C:SC:T.22B_ncl_sG3/31 g2593

M_FC - Fo_m 3190 (Rev June 1971)


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PRECEDING PAG_ BLANK NOT _[L_

TABLE OF CONTENTS

Sectlon Title PageVolume I1 INTRODUCTION i-i

i.1 PURPOSE AND SCOPE ................. 1-i-3.2 SUMMARY ......................

1.2.1 Design Goa3.s ................. 1-31.2.2 Mission Results .............. 1-9

2 SYSTEM DESIGN AND PERFOPdCA/_CE ............. 2.1-1211.i GENERAL ....................... -

2.1.1 Design Philosophy .............. 2.1-12.1-42.1.2 Wet to Dry Evolution .............

2.1.3 Overall Test Progrsm ............. 2.1-92.l-162.l.h Final Configuration Discussion ........2.1-51.1.5 Mission Performance .............2.2.1-1.2 SYST_4S .......................

2.2.1 Structural System .............. 2.2.1-12.2.2 Meteoroid Shield System ........... 2.2.2-12.2.3 Envlronmental/Thermal Control

Subsystem (E/TCS) ........ 2.2.3-12.2.h Thruster Attitu_U_n_Ve rlolS;s;_ iTi_) . 2.2.h-12.2.5 Solar Array System .............. 2.2.5-12.2.6 Electrical Power Distribution Syst_n ..... 2.2.6-12.2.7 Illumination System ............. 2.2.7-12.2.8 Communication and Data Acquisition System . . 2.2.8-12.2.9 Caution srd Warning System .......... 2.2.9-12.2.10 Experiment Accommodations Systems ...... 2._.I0-IVolume III2.2.11 Habitability Support Systems ..... : . . . 2.2.11-1

Vl me V2.2.12 Pressure Garmen_ _me_tioning System ..... 2.2.12-12.2.13 Stowage System ................ 2.2.1j-i2.2.1h Ground Support Equipment System ....... 2.2.14-12.2.15 Markings System ............... 2.2.15-1

2.3 MATERIAL USAGE AND CONTROL .............. 2.3-_

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TABLE OF CONTENTS (Continued)

Section Title PageVolume V3 RELIABILITY PROGRAM 3 1

31.1 OBJECTIVE AND METHODOLOGY .............. -3,2 RELIABILITY ..................... 3-2

3.2.1 System Reliability Analysis ......... 3-23.2.2 Design Support ............... 3-123.2.3 Production and Test Support ......... 3-21

3.3 CONCLUSIONS AND RECOI_I_ATIONS ........... 3-31

I_ SYSTEM SAFETY PROGRAM ................... _-i_.i nENERAL....................... _-I_.2 CREWSAFETY..................... h-_

_. 2.1 Concept Phase ................ _-__.2.2 Design Phase ................ _-_h.2.3 Test end Operations Phase .......... _-18

3 TRAINI_O ...................... _-28h.3.1 Skills Training ............... h-28._.3.2 Operational Training ............ h-29h.3.3 Employs Motivation/Awareness ........ h-29

_._ CONCLUSIONS AND RECOmmENDATIONS ........... _-33

5 TESTING PROGRAM ...................... 5-i5.0 INTRODUCTION .................... 5-15.1 TEST REQUIREMENTS .................. 5-5

5.1.1 General Requirezenta and Guideline8 ..... 5-55.1.2 Documentation and Control Requirements of

Component and Subsystem Testing . ...... _-75.1.3 Documentation and Control Requirements -

Spacecraft Systems and IntegratedVehicle Testing ............... 5-11

5.1._ Documentation and Control Requirements -Minion Support Testing........... 5-18


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Section Title Page5.2 COMPONENT AND SUBSYSTEM TESTING ............ 5-21

5.2.1 Development and QuaLification Testing ..... 5-,5.2.2 Production Acceptance Tests (PAT) ....... _-4

5.3 STRUCTURES TE_TING .................. 5-hb5.h SPECIAL DESIGN SUPPORT AND VERIFICATION TESTS ..... 5-h95.5 SPACECRAFT SYSTEMS TESTING .............. 5-59

5 5 1 General 5-5_5 5 2 Structures 5-635 5 3 Environmental Control 5-6h5.5.h Electrical .................. 5-665.5.5 Instrumentation and Communications ...... 5-695 5 6 Waste Management 5-735.5.7 Solar Arr_7 System .............. 5-7h5.5.8 Refrigeration ................. 5-76

9 Ordnance Subsystem 5-78.5...............5.5.10 Pneumatic Subsystem ............. 5-795.5.11 Crew Systems ................. 5-815 5 12 Stowage 5-82 e 5.5.13 Experiments Subsystem ............. 5-835 5 14 Water 5-86

5.6 INTEGRATED VEHICLE TESTING - KSC ........... 5-875 6 1 General 5-875.6.2 Vehicle Arrival, Inspection and Vertical

Assembly 5-87 e e 5 6 3 Subsystem Verification 5-895 6 h System Verification 5-1255.6.5 Final System Tes.t and Launch ......... 5-128,,c- "I 5-13r..7 MT,_I0, _cl_?O_TTFSTIN3 . . .

5 1305 7 1 OWS Backup5 7 2 Laboratory 5-1),1 i e

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Section Title Page6 ENGINEERING PROGRAM MANAGEMENT ............... 6-1

6-16.1 PLANNING AND SCHEDULING ...............6.1.1 Design and Development ............ 6-16-36 1 2 Design Changes . 6-86.1.3 Recommendations for Future Programs .....

6.2 CONFIGURATION MANAGEMENT .............. 6-96.2.1 Configuration Identification ......... 6-9f 6-136.2.2 Configuration ControJ............

1 6.2.3 Configuration Accounting ........... 6-216 2 4 Change Traffic 6-22. . . . . . e

! 6.2.5 Conclusions and Recommendations . . . . . . . 6-247 MISSION OPERATIONS SUPPORT ................. 7-1

7 1 GENERAL 7 1 _ q_ --i 7.2 MDAC-W SUPPORT AT MSFC ................ 7-3

7.2.1 Overview of MDAC-W's Role at MSFC ...... 7-37.2. ? MDAC-W/MSFC Mission Support Interface .... 7-_7.2.3 Facility Definition ............. 7-67.2.k MSFC Skylab Data System ........... 7-97.2.5 MDAC-W Support Structure and ManningSchedules 7 1_ . --7.2.6 Action Request Flow ............. 7-15

7.3 MDAC-W SUPPORT AT HUNTINGTON BEACH .......... 7-1873.1 Overview................... 7-187.3.2 Mission Support Teem Definition/Organlzatlon . 7-187.3.3 Statuary of Huntington Beach PrelaunchOperationJ Support 7 19 o . --7.3._ Identification and Management of OWS

Problems/Action Request s ........... 7-23

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Section Title Pa6e7.3.5 Sugary of Mission Support Action Items 7-257.3.6 Facility Description/Evaluation .... 7-317.3.7 Mission Support Manning Schedules(mmnealUnnana) .............. 7-37

7._ CONCLUSIONS AND RECO_4mrDATIONS ........... 7-_37. _. 1 General ................... 7-_7. _. 2 PTelaunch Support .............. 7-_7._.3 Mission Steulations ............. 7-_37.I*._ Mission Support Organizstion and Manning . . . T-_7. _. 5 Mission Support Facilities .......... 7-47._.6 Action Item Ansi_ent, TTacking and Response 7-457._.7 Hardware and Test Support .......... 7-467._.8 MDAC-WOn-Site Support st MSFC ........ 7-47

8 _ TECH_0LOGY ....................... 8-18,1 AEROSPACE APPLICATIONS ................ 8-1

8.1.1 New Technology P&tent Disclosures ...... 8-18.1.2 Applic&ble Hardware and Design Approaches . . 8-1

8.2 OTHER APPLICATIONS .................. 8-228.2.I Electronic/Electrical ............ 8-2_8.2.2 Fireproo _ "*ale ............. 8-258.2.3 Zero Grsvtty Restre/nt Equipment ....... 8-268.2. _ Structural Technology ............ 8-268.2.5 Fire Detection, Prevention and Suppression . . 8-278.2.6 Bioelde Wipes ................ 8-278.2.7 Therm_ Mec)_mical .... . ......... 8-288.2.8 Potlble Water 8terili_tion . . ....... 8-288.2.9 Noise Control ................ 8-288._._0 Pneu_tic Valve _sign ............ 8-298.2.11 Produet Ssfety Eealuation . . . . ...... 8-29


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Section Title Pag9 CONCLUSIONS AND P_ECO_4ENDATIONS .............. 9-i

9.1 MISSION PERFORMANCE ................ _-_9.1.1 Structural System .............. 9-19.1.2 Meteoroid Shield (MS) ............ 9-59.1.3 Thermal Control System (TCS) ......... 9-59.1._ Thruster Attitude Control System (TACS) 9-79.1.5 Solar Array System (SAS) ........... 9-89.1.6 Electrical Power Distribution System (PDS; . . ,_-9.1.7 Illumination System ............. 9-19.1.8 Ccmmunicatlon and Data Acquisition Systems(DAS).................... 9-9.1.9 Caution and Warning (C&W) System ....... 9-19.1.10 Experiment Accomn_tions Systems ...... 9-19.1.11 Habitability Support Systems (HSS's) ..... 9-19.1.12 Pressure Garment Conditioning System ..... 9-29.1.13 Stowage System ................ 9-29.1.1_ Marking System ................ 9-2

9.2 PROGRAM PLAR_ING ................... 9-29.2.1 Organization ................. 9-29.2.2 Establxshing Requiremente .......... 9-9.2.3 Controlling to Requirements ......... 9-29.2._ Improvements for Future Programs ....... 9-

9.3 TESTING ....................... 9-39.3.1 Development and Q_allficatlon ........ 9-39.3.2 Spacecraft Syst_ Testing .......... 9-39.3.3 Conclusioas and Ree_endation8 ....... 9-_

9._ PRELAUNCH AND MISSION SUPPORT ............ 9-_I0 BIBLIOGRAPHY 10-!

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FIGURES

i_umbe._r1.2.i-i Skylab Orbiting Assembly l-hi._'.1-2 Skylab - Function of Modules 1-5I.2.1-3 Orbital Workshop I-7i.2.1-4 Mission Design Profile I-,_1.2.2.5-1 Mission Actual Profile i ,132.,.l-1 S-IV-Gemini Space Laboratory Concept 2.1-22.1.2-1 NASA Saturn S-IVB Orbital Workshop 2.1-52.1.2-2 Wet Workshop Launch Configuration 2.1-72.1.h.l-1 Orbital Workshop T__k Assembly, Skirts and 2.1-17

Interstage2.1.4.2-1 Meteoroid Shield 2.1-192.1.h.3-1 Active Thermal Control System 2.1-212.1.h.4-1 Thruster Attitude Control System 2.1-232.1.4.5-1 Solar Array System 2.1-252.1.h.6-1 Electrical Power Distribution System 2.1-272.I.h.7-1 Ill_nination System 2.1-292.I.h.8-1 Communications System 2.i--302.1.h.8-2 Data Acquisition System 2.1-322.I. h.8-3 Electrical Comms_d System 2.1-332.1. h.9-1 Caution and Warning System 2.1-3h2.i.h.10-1 Waste Management System 2.1-362.i.h.10-2 Waste Management System Trash Disposal 2.1-372.1. h.10-3 Water System 2.1-392.l.h.lO-h Personal Hygiene and Body Cleansing System 2.1-412.l.i_.10_5 Food Manac_rn_,ntSystem 2.l-h-2.I.h.10-6 Sleep _uppor_ System 2.l-h_2.i.h.!O-7 Refrigeration System 2.l-h52.i.4.ii-i Stowage System 2.1-472. ].)A.2-1 Waste )4an_gemen_ Vac'numProvinlcnz ?.l-h9

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Number Page2.2.1.2-21 WMC Closeout at Floor 2.2.1-712.2.1.2-22 Closeouts Between Floor and Ceiling 2.2.1-Fz2.2.1.2-23 Closeouts on Aft Floor 2.2.1-742.2.1.2-2h Forward Floor Colseouts ;.2.1-(_2.2.i.2-25 Water Tank Closeouts "-_..."tI'2.2.1.2-26 Wardroom Entry Curtain "2? I ,,2.2.1.2-27 Crewman Restraints - Internal 2.2. ].-792.2.1.2-28 Astronaut Aids (Platform Foot Restraints) 2.2 1-8!2.2.1.2-29 Astronaut Aids (Light Duty Foot Restraints) 2 2.1-822.2.i.2-30 Footwell Restz aints 2.2.I-P),2.2.1.2-31 Triangle Shce 2.2 i..3o2.2..l.-32 Crewman Fixed Hand Restraints (Internal) 2.2.1-882.2.1.2-33 Dome Ring Locker Lower Leg Restraint 2.2.1-922.2.1.2-34 Table Restraints (Triangle Shoe) Test 2.2.1-i1(

Configuration2.2.1.2-35 Table Restraints (Fixed Foot Restraint) Test 2.2.1-111

Configuration2.2.1.2-36 Triangle Shoe Test Configuration 2.2.1-1122.2.1.2-37 Pelvic _estraint Test Configuration ?.2.l-lib,2.2.1.3-1 Aft Structure 2.2.1-1382.2.i.3-2 TACS Gas Storage Sphere Installation Subsystem 2.2.1-1392.2.1.3-3 TACS Gas Storage Sphere Installation Subsystem 2.2.l-lh02.2.1.3-4 TC-9 Test Specimen 2.o..i-i_I2.2.1.3-5 TACS Sphere Meteoroid Shield Installation 2.2.1-1 hh2.2.1.3-6 TACS Sphere Meteoroid Shield and Skirt 2.2.1-Ih52.2.1.3-7 Aft Structure - Radiator Support Structure 2.2.1-1462.2.i.3-8 Radiator Sandwich Construction 2.2. l-lh82.2.i.3-9 Radiator - Thrust Casting Connection 2.2. l-lh92.2.1.3 i0 Thermal Control Unit Installation 2.2.1-1502.2.1.3-11 Thermal Control Unit Installation 2.2.1-1512.2.i.3-12 Radiator Impingement Shield 2.2.1-1532.2.i.3-13 Radiator Shield Jettison Mechanism 2.2. I-.1552.2.I.3-I4 Plu,.eimIin_c,L,,t Curtala 2.2. i-1'5(,2.2.1. _-i Aft Interstate Buic Struc%ure 2,2.1-1692.2.i.h-2 Ring Frames and Intercoatals 2.2.1-1702.2.1.h-3 Baslc Shell Structure - Aft Interstage 2.2.I-17J

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Number2.2.l.h-h Basic Shell Structure - Aft Interstage - Vent 2.2.1-i'[3

Openings 2.2.1.4-5 Basic Shell Structure Aft Interstage . _ '_h

2.2.1.4-6 Aft Inte_stage/GSE Interfaces 2 _2.2.i.h-7 Basic Shell Structure Aft Inters tage ,22.2.2.1-i Meteoroid Shield '_-_,'!_2.2.2.1-2 Meteoroid Shield Panel Joint .....L-,,2.2.2.1-3 Meteoroid Shield Boot 2.2.2-'(2.2.2.l-h Meteoroid Shield Auxiliary Tunnel Frame and "2.2.':-9Beaded Panel Cover

2.2.2.1-5 Meteoroid Shield Deployment Ordnance and l,'oldout _ ,: :Panels_ 2.2.2.1-6 Meteoroid Shield :._..2-J2

2.2.2.1-7 Deployable Meteoroid Shield 22._ i32.2.2.1-8 Meteoroid Shield Rigging Device 2.2.2. IlL2.2.2.1-9 Meteoroid Shield Release System z.2,2-1'(2.2.2.1-10 Shield Release Device 2.2.2-182.2.2.1-11 Meteoroid Shield Release Mechanism 2.2.2-192.2.2.2-1 Workshop Flight Systems 2.2.2-392.2.2.2-2 Forward Dome Structural Con figurat ions 2.2.2-hl2.2.2.2-3 Airlock Cutout Impact Angles 2.2.2-_22.2.2.2-h End Closure Configurati on 2.2.2-h32.2.2.2-5 Aft Dome/Skirt Configurations 2.2.2-hh2.2.2.2-6 Skylab Configuratlon 2.2.2- 452.2.2.2-7 Meteoroid Damage Probabilities 2.2.2-492.2.2.2-8 Meteoroid Shield Paint Pattern 2.2.2-522.2.3-1 Crew Cm_fort Criteria 2.2.3-52.2.3-2 Maximum Dynamic Input to PLV Fan/Shroud Asse_t[y 2.2.3-i1(In all Three Axes)2.2.3-3 VCS Schematic 2.2. _-_0, r_2 2.3-h Alrlock to Workshop Interface and Mixing Chamb_.: _.2.3-_2

2.2.3-5 Ventilation 2.2.3-2_2.2.3-6 Fan Inlet Duct 2 _ 3 21.2.2.3-7 Duct Diffuser _.c. _--2o2.2.3-8 Fen Cluster sad Muffler Assembly 2.2.3-272.2.3-9 OWS Ven*J lation System Fan Cluster Assembly _.2.3-,_2.2.3-10 Duct Fan 2.d j-dj

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Number Page2.2.3-11 Floor/Air Diffuser Arrangement 2.2.3-312.2.3-12 Sleep Area Air Outlet 2.2.3-322.2.3-13 Ventilation Control System Diffuser Locations 2.2.3.-332.2.3-14 Portable Fan with Sound Suppression 2.2.3-322.2.3-15 Circuit Breaker Panel 61h 2.2.3-362.2.3-16 Fan Control 2.2.3-3?2.2.3-17 Fan Bus Selection 2.2.3-382.2.3-18 Convective Heater 2.2.3-402.2.3-19 Control and Display Panel 617 Thermal Control 2.2.3-42

System2.2.3-20 Heater Control 2.2.3-4_2.2.3-21 Heater Control Duct 3 2.2.3-452.2.3-22 Radiant Heaters 2.2.3-472.2.3-23 Radiant Heater - IB81046 2.2.3-482.2.3-24 Radiant Heater Components 2.2.3-492.2.3-25 ECS Control Panel 203 2.2.3-512.2.3-26 Radiant Heater Control 2.2.3-522.2.3-27 OWS View Window Design Criteria 2.2.3-532.2.3-28 Wardrooa Window 2.2.3-542.2.3-29 Wardroom Window 2.2.3-552.2.3-30 Wardroom Control and Display Panel 700 (IB84376-I) 2.2.3-572.2.3-31 Wardroom Window Heater Electrical Schematic 2.2.3-582.2.3-32 Thermal Control System Schematic 2.2.3-602.2.3-33 Preinstailed High Performance Insulation 2.2.3-632,2.3-34 Forward Dome High Performance Insulation 2.2.3-642.2.3-35 High Performance Insulation Purge System 2.2.3-662.2.3-36 External Paint Pattern 2.2.3-702.2.3-37 External White Paint Pattern 2.2.3-712.2.3-38 Thermal Radiation Coating 2.2.3-732.2.3-39 Meteoroid Shield Boot 2.2.3-742.2.3-40 Forward Thermal Shield 2.2.3-75_..2.l-dl Aft Thermal Shield 2.2.3-762.2.j-42 JSC 't_ro_ol ConA'igu/'ation 2.2.3-792.2.3-43 MSFC Solar Sall Configuration 2.2.3-802.2.3-44 OWS Heat Pipe Wick Conflguratl)n 2.2.3-832.2.3-45 Heat P_pe Location_ 2.2.3-84

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l_umber Page2.2.3-h6 Heat Pipe Installation at Water Bottle/Balsa Wood 2.2.3-852.2,3-h7 Heat Pipe Installation at Floors 2.2.3-872.2.3-48 Heat Pipe Support Assembly 2.2.q-882.2.3-49 Heat Pipe Installation 2.2.3-912.2.3-50 OWS Viewing Window Cold Coating Test Results 2.2.3-102.2.3-51 SL-I Forward Compartment Wall Boost Temperature 2.2.3-10

History, Sensor C70342.2.3-52 SL-I Forward Compartment Wall Boost Temperature 2.2.3-10

Histe:y, Sensor C70h52.2.3-53 SL-1 Forward Compartment Wall Boost Temperature 2.2.3-10

History, Sen_or C70h7.....3-51_ SL-I Aft Compartment Wall Boost Temperature 2.2.3-10

History, Sensor C70532.2.3-55 SL-I Forward Skirt Thermal Shield Boost Temperat re 2.2.3-11

History, Sen._or C71852.2.3-56 SL-I Aft Skirt Thermal Shield Boos_ Temperature 2.2.3-11

History, Sensor C71772.2.3-57 Wardroom Window Daily Temperature Extremes 2.2.3-i12.2.3-58 OWS Aft Skirt Transducer C7189 Location 2.2.3-122.2.3-59 Estimated Retro-Rocket Plume Contamination 2.2. ?-132.2.3-60 Correlation of Temperature Data for S-13G Painted 2.2.3-13Aft Skirt2.2.3-61 Aft Skirt Maximum Orbital Temperatures at Beta = 0 2.2.3-13

Deg, Sensor _7189) 2.2.3-62 S-13G White Paint Degradation 2.2.3-13

2.2.3-63 Temperature Response of Gold Taped Sidewall to 2.2.3-1hDirect Solar Exposure

2.2.3-6h OWS External Wall Temperature SimulatAon for EREPS 2.2.3-1h31 and 322.2.3-65 OWS External Wall Temperature Simulation for EREP 2h 2.2.3-142.2.3-66 Tank Wall Optical Properties 2.2.3-ih2.2.3-67 OWS Mean Internal and Floor-Stowed Food Tempera- 2.2.3-15

ture History, DOY's 13.5- lh72.2.3-68 OWS Rack-Stowed Food Temperature History, DO_ 's 2.2.3-1_135 - lh72.2.3-69 OWS Film Vault Temperature History, DOY's 135 - lh7 2.2.3-152.2.3-70 OWS Mean n_ernal Temperature History, DOY's 2.2.3-16

I)_7 - 15_

DOY's lh7 - 15_

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Number Page2.2.3-72 OWS Film Vault Temperature History, DOY's 147 - 155 2.2.3-1632.2.3-73 SL-2 Urew Comfort Conditions 2.2.3-1642.2.3-74 OWS Cooldown After Parasol Deployment 2.2.3-1652.2.3-75 SL-2 External Surface Temperature Distribution 2.2.3-1672.2.3-76 OWS Mean Internal Temperatu_e History, DOX's 2.2.1-169

148- 1742.2.3-77 OWS Temperature During the First Storage Period, 2.2.3-171DOY's 173 -,2092.2,3-78 OWS Maximum and Minimum Internal Temperatures, 2.2.3-172DOY's 210 - 2682.2.3-79 SL-3 Crew Comfort ConditJ ons 2.2.3-1742.2.3-80 OWS Surface Temperatures for a Single EREF Maneuver 2.2.3-1772.2.3-81 OWS Surface Temperatures for Back-to-Back EREP 2.2.3-178Maneuvers2.2.3-82 OWS Temperatures During the Second Storage Period 2.2.3-180DOY's 268 - 3202.2.3-83 SL-4 Maximum and Minimum Mean Internal Temperatures 2.2.3-1822.2.3-84 SL-4 Crew Comfort Conditions 2.2.3-1842.2.3-85 OWS Tank Wall Temperature Response During EREP's 2.2.3-187

29 and 30 (DOY 014)2.2.3-86 OWS Structural Temperature Transducer Locations 2.2.3-1932.2.4.1-1 TACS Minimum Thrust Versus Total Impulse Consumed 2.2.4-32.2.4.2-1 TACS Schematic 2.2.4-42.2.4.2-2 TACS - Component Locations 2.2.4-52.2.4.2-3 TACS Installation 2.2.4-62.2.4.P-4 TACS Control Valve 2.2.4-72.2.4.2-5 Typical Detail of Brazed Joint 2.2.4-92.2.4.2-6 TACS Bimetallic Joint 2.2.4-102.2.4.4-1 Skylab TACS Usage 2.2.4-162.2.5.2-1 Solar Array Wing Assembly 2.2.5-42.2.5.2-2 Solar Cell Module 2.2.5-52.2.5.2-3 Orbital Workshop SAS - Electrical Power 2.2.5-72.2.5.2-4 SAS Beam/Fairing Skirt Attach Point 2.2.5-82._.5.2-5 Wing Section Retention ;_d _elease System 2.2.5-102.2.5.4-1 OWS Solar Array Performance 2.2.5-372.2.5.4-2 SAG Performm_ce - SAG 1 and SAG 2 2.2.5-39(DOY's159, B = i0)2.2.5.4-3 SAG Performance - SAG's 3 and 4 (DOY 159, 8 = i0) 2.2.5-40


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i Number Page2.2.5.4-4 SAG Performance - SAG's 5 and 6 (DOY 159, B = I0e) 2.2.5-412.2.5.4-5 SAG Performance - SAG's 7 and 8 (DOY 159, 8 = lO) 2.2.5-422.2.5.4-6 SAG Performance - SAG 1 (DOY 175, 8 --+ 73.5) 2.2.5-43

I 2.2.5.4-7 SAG 1 Voltage, DOY 339, Beta = -9 2.2.5-442.2.5.4-8 SAG 1 Current, DOY 339, Beta = -9 2.2.5-45

I 2.2.5.4-9 SAG's 1 and 2 Voltage, DOY 034, Beta = 0 2.2.5-462.2.5.4-10 SAG's 3 and 4 Voltage, DOZ 034, Beta = 0 2.2.5-472.2.5.h-1: SAG's 5 and 6 Voltage, DOY 034, Beta = 0 2.2.5-482.2.5.4-12 SAG's 7 and 8 Voltage, DOY 034, Beta = 0 2.2.5-492.2.5.4-13 SAG's 1 and 2 Current, DOY 034, Bets = 0 2.2.5-502.2.5.h-14 SAG's 3 and 4 Current, DOY 034, Beta = 0 2.2.5-512.2.5.4-15 SAG's 5 and 6 Current, DOY 034, Beat --0 2.2.5.-522.2.5.4-16 SAG's 7 and 8 Current, DOY 034, Beta = 0 2.2.5-532.2.5.4-17 Solar Array/Temperature Transducer Temperature 2.2.5-_6Differential (Beta --0)2.2.5.4-18 Solar Arra_/Temperature Transducer Temperature 2.2.5-57

Differential (Beta = 73.5)2.2.5.4-19 SAG Characteristics - 15 Modules DOY 159; SAG's 2.2.5-58

i, 2, 3, 4, and 72.2.5.4-20 SAG Characteristics - 14 Modules DOY 159; SAG's 2.2.5-59

5and82.2.5.4-21 SAG Che_acteristics - 13 Modules DOY 159; SAG 6 2.2.5-602.2.5.4-22 SAS Transducer Thermal Profile (DOY 159, Beta = 2.2.5-6__

I0)2.2.5.4-23 SAS Transducer Thermal Profile (DOY 175, Beta = 2.2.5-65

+73.5 )2.2.5.h-24 SAS Transducer Thermal Profile (DOY 339, Beta = 2.2.5-66-9)2.2.5.4-25 SAS Transducer Thermal Profile (DOY 034, Beta = 2.2.5-670 )2.2.5.4-26 Typical SAS Thermal Profile (Actual vs Predicted) 2.2.5-682.2.5.4-27 SAS Temperature Transducer Measurement History 2.2.5-702.2.6.1-1 Zero G Connector - Disengaged 2.2.6-102.2.6.1-2 Zero G Connector - Engaged 2.2.6-112.2.6.2-1 Rigl d Trough 2.2.6-172.2.6.2-2 Flex Trough Usag_ (General Concept) 2.2.6-182.2.6.2-3 Closed Trough System (General Concept) 2.2.6-192.2.7.2-1 OWS Floodlight Locations and Marking 2.2.7-7


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Number Page2.2.7.2-2 Remote Lighting Switch Panel 616 2.2.7-82.2.7.2-3 Remote Lighting Switch Panel 630 2.2.7-92.2.7.2-I_ Circuit Breaker Panel - 613 Lighting 2.2.7-102.2.7.2-5 Floodlight Assembly Detail 2.2.7-162.2.7.2-6 Exploded Floodlight Assembly 2.2.7-172.2.7.2-7 Floodlight Cross Section 2.2.7-182.2.7.2-8 Portable Lighting 2.2.7-202.2.7.6-1 Floodlight as Originally Proposed- In Force 2.2.7-37

Until December 12, 19692.2.7.6-2 Pictorial History of iB6936h Floodlight Design 2.2.7-382.2.7.6-3 Floodlight Design in Force From January 15, 1970 2.2.7-40

Until February 13, 19702.2.7.6-h Floodlight Design in Force Since February 13, 1970 2.2.7-h22.2.8.1-I "Ring" Bus Circuit Concept 2.2.8-52.2.8.1-2 Communi cation Box 2.2.8-72.2.8.i-3 Communi cations System Wiring Concepts 2.2.8-162.2.8.2-1 OWS Signal Conditioning Power 2.2.8-272.2.8.2-2 OWS DAS Heater Power 2.2.8-282.2.8.2-3 Telemetry System Schematic 2.2.8-292.2.8.h-1 Sequence No. C6 2.2.8-,52.2.9.2-1 Fire Sensor Control Schematic 2.2.9-82.2.9.2-2 Control and Display Panel 616 - Caution/Warning 2.2.9-11

System2.2.10.1-1 OWS Experiment Accommodations - Experiment 2.2.10-9Location2.2.10.1-2 OWS Experiment Accommodations - Experiment 2.2.10-10Location2.2.10.1-3 Experiment Accommodations Typical Floor Mounting 2.2.10-11Provisions2.2.10.1-!_ SAL Tripod 2.2.10-122.2. I0.1-5 Water Pressurization Network 2.2.10-152.2.10.1-6 Water Pressurization Panel 2.2.10-162.2.10.1-7 Water Pressurization Network 2.2.10-172.2.10.1-8 ESS _._Supp y Panel 2.2.10-182.2.10.1-9 OWS Experiment Accommodations Vacuum System - 2.2. i0-19

Experiments2.2.10.1-10 Redesigned LBNPD Vacuum System 2.2.10-212.2.10.2-1 Film Vault 2.2.10-35


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Number Page2.2.10.2-2 Film Vault 2.2.10-362.2. lO.2-3 Film Vault 2.2.10-372.2. i0.3-1 Solar Flare Notification System 2.2.lO-h52.2.10.4-1 Scientific Airlock (SAL) Design Requirements 2./.lO-j0

Summary2.2.i0. h-2 Scientific Airlock Installation 2.2.lO-Sh2.2.10. h-3 SAL Window Container 2.2.10-562.2.10.5-1 -Z Scientific Airlock Filter and Desiccant 2.2_10-66

Equipment2.2.10.5-2 +Z Scienti fic Airlock Filter Equipment 2.2.10-672.2.10.5-3 SAL Repressuri zation Subsystems 2.2.10-702.2.11.1-1 Maximum Urine Delivery Rate 2.2.11-72.2.11.1-2 Proof Pressure Tests 2.2.11-182.2.11.1-3 Trash Disposal Subsystem Trash Bag Locations 2.2.11-2h2.2.ii. 1-h Trash Disposal Airlock Sequential Operation 2.2.11-252.2.11.i-5 Trash Lock Loading Equalize Pressure 2.2.11-262.2.11.I-6 Trash Lock Trash Bag Eject 2.2.11-272.2.ii.1-7 Waste Management Schemat ic 2.2.11-292.2.11.1-8 Skylab - Orbital Workshop DCR HSS Waste Manage- 2.2.11-30

ment Subsystem2.2.ll.1-9 Waste Management Subsystem 2.2.11-312.2.11.1-10 hO00 ML - Urine System Volume Determinator Stowage 2.2.11-322.2.11.1-11 Waste Management Subsystem 2.2.11-332.2.11.I-12 Waste Management Collection 2.2.11-3h2.2.11.i-13 Waste Management Subsystem Fecal Collection Bag 2.2.11-362.2.11.i-14 Fecal Collector - Functional Diagram 2.2.11-372.2.11.i-15 Skylab - Orbital Workshop Collection Bag Usage 2.2.11-39Stheme2.2.11.1-16 Waste Management Subsystem Fecal Contingency Bag 2.2.11-402.2.11.1-17 Urine Collection and Sampling Equipment 2.2.11-h32.2.11.1-18 Waste Management Subsystem Debris Collection Bag 2.2.11-_72.2.11.i-19 Trash Disposal Subsystem Trash Bag Locations 2.2.11-h92.2.11.I-20 Trash Collection Bags 2.2.11-502.2.ll.l-21 Fecal/Urlne Collector 2.2.11-542.2.11.i-22 Fecal/Urine Collector - Block Diagram 2.2.11-552.2.11.1-23 Fecal and Urine Collection Facilities 2.2.11-572.2.11.1-2h Fecal/Urlne Collector 2.2.11-60


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Number Page2.2.11.1-25 Fecal/Urine Collector - Schematic 2.2.11-612.2.11.1-26 Typical Urine Drawer - Schematic 2.2.11-622.2.11.1-27 Urine Chiller - Functional Diagram 2.2.11-642.2.11.1-28 Urine Separator - Exploded View 2.2.11-oL,2.2.11.i-29 Waste Management Subsystem 2.2.11-722.2.11.1-30 Waste Processor Chamber 2.2.11-732.2.11.1-31 Waste Processing and Urine Management Facilities 2.2.11-762.2.1!.1-32 Waste Processor - Functional Diagram 2.2.11-772.2.11.i-33 Urine System Dump Compartment 2.2.11-81

" 42.2.11._.-3 Waste Management System Fecal and Urine Return 2.2.11-83Containers2.2.11.i-35 Vacuum Cleaner Assembly 2.2.11-862.2.11.1-36 Vacuum Cleaner and Accessories 2.2.11-872.2.11.1-37 Trash Airlock 2.2.11-902.2.11.i-38 Urine Collection Drawer Seal Debondlng - Second 2.2.11-142Mission2.2.11.1-39 Daily Urine Volume (Mechanical vs LI Analysis) - 2.2.11-156First Mission2.2.11.1-40 Dail> Urine Sample Size - First Mission 2.2.11-1572.2.11.1-41 Daily Urine Volume (Mechanical vs LI Analysis) - 2.2.11-160Second Mission2.2.11.1-42 Daily Urine Sample Size - Second Mission 2.2.11-1612.2.11.2-1 Wardroom Food Reconstitution Waste Dispensers 2.2.11-1902.2.ii.2-2 Water Dispenser 2.2.11-1912.2.Ii.2-3 Rehyara_ion Backup Provision (Drinking Water 2.2.11-192

Dispenser)2.2.ii.2-4 Water System 2.2.11-1952.2.11.2-5 Potable Water System Schematic 2.2.11-1972.2. ll.2-6 WMC Water System Schematic 2.2.11-1982.2. ii.2-7 Water Storage Provis ions 2.2.11-2012.2.11.2-8 Water Tank - Schematic (Typ) 2.2.11-2022.2.Ii.2-9 Pump Assembly Water Agitator 2.2.ll-20h2.2.11.2-10 Water Tank Heater Blanket - Schematic (Typ) 2.2.11-205......3..2-11 Potabit:U,._.c,... S._h,.,:_atc 2.2.11-2072.2.11.2-12 Water Pressurization Panel 2.2.11-2102.2.11.2-13 Pressure Regulator 2.2.11-211?.2.11.2-14 Water Pressurization Network 2.2.11-212

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Number Page2.2.11.2-15 Water Pressurization Network 2.2.11-2132.2.11.2-16 Water Pressurization Network 2.2.11-2142.2,ll.2-17 ESS N2 Supply Panel 2.2.11-2162.2.11.2-18 Hoses 2.2.11-_1[2,2.ii.2-19 Hose Restraint 2.2. ll-212.2.11.2-20 Wardroom and WMC Water Port - Urine Flush Port 2.2.11-21_2.2.11.2-21 Wardroom Water Network 2.2.11-2202.2.ll.2-22 Wardroom and WMC H20 Heaters 2.2.11-2222.2.11.2-23 Water Heater - Functional Diagram 2.2.11-2232.2.11.2-24 HSS Water System Water Chiller 2.2,11-2252.2.11.2-25 Water Chiller - Functional Diagram 2.2,-1-2262.2.11.2-26 Water Management Dispensers - Installation 2.2.11-2282.2.11.2-27 HSS Food Reconstitution Water Dispenser 2.2.11-2302.2.11.2-28 HSS Water Subsystem Drinking Water Dispensers 2.2.-1-2322.2.11.2-29 Water Subsystem Drinking Water Dispenser 2.2.11-234Instal] ation2.2.11.2-30 WMC Water Supply Network 2.2.11-2362.2.11.2-31 Urine Flush Dispenser 2.2,11-2382.2.11.2-32 Personal Hygiene Water Dispenser 2.2.11-2422.2.11.2-33 Partial Body Cleansin_ Facilities - Handwasher 2.2.11-2432.2.11.2-34 Washcloth Squeezer Bag 2.2.11-2452.2.11,2-35 Vacuum D_,_p and Vacuum Exhaust Systems 2.2.11-2472.2.11,2-36 Wardroom Vacuum Outlet - Water Dump 2.2.11-2482.2.11.2-37 Dump Heater Probe 2.2.11-2502.2.11.2-38 Vacuum Provision Schematic (Typ) 2.2.11-2512.2.11.2-39 WMC Vacuum Outlet Water Dump 2.2.11-2522.2.11.2-h0 Water Purification Equipment 2.2.11-2552.2.11.2-41 Water Sampler 2.2.11-2562.2.11.2-42 Reagent Container Assembly 2.2.11-2582.2.11.2-43 Color Comparator 2.2.11-2592.2.11.2-hh Water/Iodine Waste Sample Container P/N IB80557 2.2.11-2612.2.11.2-h5 Iodine Addition Chart 2.2.11-2632.2.11.2-46 iodine Contalner 2,2.ii..22.2.11.2-47 Iodine Injector 2.2.11-2652.2.11.2-_8 Water Deionization Filter Assembly 2.2.11-2672.2.11.2-49 Portable Water J.:_tem S ::uumatic 2.2.11-271

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Number Page2.2.11.2-50 WMC Water System Schematic 2.2.11-2722.2.11.2-51 Water Usage - Skylab 2.2.11-29h.12.2.11.2-52 Water Consumption - Tank i, SL-2, Wardroom 2.2.11-2952.2.11.2-53 Water Consumption - Tanks lO and 2, SL-3, Wardroom 2.2.11-29L,2.2.11.2-54 Water Consumption - Tanks 2, 3, 4, and 5, SL-h 2.2.11-2972.2.11.2-55 Water Usage - Tank 7, SL-3, Personal Hygiene 2.2.11-2_,b2.2.11.2-56 Water Usage - Tanks 7 and 8, SL-h, Personal Hygiene 2.2.11-2992.2.11.2-57 Daily Drinking Water Consumption, CDR - SL-2 2.2.11-3002.2.11.2-58 Daily Drinking Water Consumption, SPT - SL-2 2.2.11-3012.2.11.2-59 Daily Drinking Water Consumption, PLT - SL-2 2.2.11-30P2.2.11.2-60 Daily Drinking Water Consumption, CDR, SL-3 2.2.11-3032.2.11.2-61 Daily drinking Water Consumption, SPT - SL-3 2.2.11-3042.2.11.2-62 Daily Drinking Water Consumption, PLT - SL-3 2.2.11-3052.2.11.2-63 Daily Drinking Water Consumption, CDR - SL-4 2.2.11-3062.2.11.2-6h Daily Drinking Water Consumption, bl_1- SL-4 2.2.11-3072.2.11.2-65 Daily Drinking Water Consumption, PLT - SL-4 2.2.11-3082.2.11.2-66 Water Tank No. 1 Iodine Depletion 2.2.11-3122.2.11.2-67 Water Tank No. 2 Iodine Depletion 2.2.11-3132.2.11.2-68 Water Tank No. 3 Iodine Depletion 2.2.11-3142.2.11.2-69 WaZer Tank No. h Iodine Depletion 2.2.11-3152.2.11.2-70 Water Tank No. 5 Iodine Depletion 2.2.11-3162.2.11.2-71 Water Tank No. 6 Iodine Depletion 2.2.11-3172.2.11.2-72 Water Tank No. 7 Iodine Depletion 2.2.11-3182.2.11.2-73 Water Tank No. 8 Iodine Depletion 2.2.-1-3192.2.11.2-74 Water Tank No. 9 Iodine Depletion 2.2.11-3202.2.11.2-75 Water Tank No. l0 Iodine Depletion 2.2.11-3212.2.11.2-76 OWS Iodine Solution for Water Purification 2.2.11-3252.2.11.2-77 OWS Reagent for 12 Determination 2.2.11-3272.2.11.2-78 OWS i Water Heater Resistance vs Days 2.2.11-346

Operating2.2.iI. 3-1 Personal Hygiene Equipment 2.2.11-3822.2.11.3-2 Gener_l P,rpnze Tlz_ue/Soap D_spenser 2.2.11-38_,2.2,ii.3-3 Towel an_ Washcloth D_spenser 2.2.11-3892.2.ii.3-4 Washcloth/Towel Drying Area 2.2.I1-3912.2.11,3-5 Personal Hygiene Kit 2.2.11-3922.2.ii.3-6 WMC/SI _er _ L_.: ::[:_",rLocc:';i:,: I- _9._,or.i. ct " 2,2.1 _' '

XXi


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Number Page2.2.ii. 3-7 WMC Water Module 2.2.11-3952.2o11.3-8 WMC Water Dispenser/Squeezer 2.2 11-3962.2.ll. h-1 Location of Personal Hygiene Equipment 2.2. ll-hl22.2.ii. 4-2 Whole Body Shower (Operational) 2.2. i-4_42.2.11.4-3 Shower Centril%_g_C Concept 2 ? L!-.4]52.2. ii.5-1 Ambient Food Storage "2.. Li-4352.2. ii.5-2 Ambient Food Supply - Daily 2.2.11-4q62.2. ll.5-3 Galley 2.2. ll- 4382.2. ll.5-4 Food Table and Restraints 2.2.11-4402.2.11.6-1 Sleep Compartment Equipment 2 o.11_4492.2.ll.6-2 Blanket and Pillow Installation 2.'2.1!-4522.2.ll.6-3 Sleep Compartment Light Baffles 2.2.ll-h572.2.ll.7-1 Refrigeration System Schematic 2.2.11-4732.2.iI.7-2 Refrigeration System 2.2.ll-4742.2.ll.7-3 Refrigeration Subsystem Installation 2.2. ll- 475

' 2.2. ii.7-4 Refrigeration Subsystem Radiator. 2.2.11-4762.2.ll.7-5 Refrigeration System Radiator Bypass Valve 2.2.11-4782.2.ll. 7-6 Refrigeration System Radiator Relief Valve 2.2.11-479

13896132.2. ll.7-7 Refrigeration System Urine Free zer 2.2.11-4812.2.11.7-8 Refrigeration System Food Freezer 2.2.11-4822.2.11.7-9 Refrigeration Subsystem Chiller Control Valve 2.2.11-4832.2.ii. 7-10 Refrigeration System Regenerator 2.2.11-4842.2.11.7-11 Refrigeration Subsystem Regenerator Heater 1B853_7 2.2.11-4852.2. ll.7-12 Water Chiller 2.2.11-4862.2.11.7-13 Centrifugal Separator System Chiller Compartment 2.2.11-487Details2.2.11.7-14 Refrigeration Subsystem Pump Pa_ks4_e 2.2.11-4882.2.1] .7-15 Refrigeration System Pump 2.2.11-4892.2.11.7-16 Refrigeration System Pump Relief Valve 2.2.11-4902.2.11.7-17 Refrigeration Subsystem Filter (15 M) 2.2.11-h922,2.11.7-18 RS Performance Data Daily Minimum/Maximum - _.? ii-5h2

"L-IISL-22.2.11.7-19 RS Performance Data Daily Minimum/Maximum - 2.3.11-543

SL-.1/SL-22.2.11.7-20 RS Performance Data Daily Minimum/Maximum - 2.2.11-5hhSL-I/SL-2


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Number Page2.2.11.7-21 RS Performance Data Daily Minimumaximum - 2.2.11-545SL-1/SL-22.2.11.7-22 KS Performance Data Daily Minimum/Maximum - SL-3 2.2.11-5462.2. ii.7-23 RS Performance Oa +p Dally Minimum/Maximum - SL-3 2.2.i,_-5)2.2.11.7-24 RS Performance Data Daily Minimumaximum - SL-3 2.2.11-54o2.2.11.7-25 KS Performance Data Daily Minimum/Maxlmum - SL-3 2.2.11-5492.2.11.7-26 RS Performance Data Daily Minimum/Maximum - SL-h 2.2.11-5502.2.11.7-27 RS Performance Data Daily Minimum/Maximum - 8L-h 2.2.11-5512.2.11.7-28 KS Performance Data Daily Minimum/Maximum - SL-h 2.2.11-5522.2.11.7-29 KS Performance Data Daily Minimum/Maximum - SL-4 2.2.11-5532.2.11.7-30 SL-I Refrigeration System Data - Launch +6 Hours 2.2.11-555G.E.T.2.2.11, _-31 KS - Food Temp History (DOY 136) 2.2.11-5582.2.11.7-32 RS - Food Temp History (DOY 137) 2.2.11-5592.2.11.7-33 Radiator Bypass Valve Cycle 2.2.11-5602.2.11.7-34 KS Performance Trend Data (Pre-act/Act/Post Act) 2.2.11-5612.2.11.7-35 RS Performance Trend Data 2.2.11-5622.2.11.7-36 RS Performance Trend Data 2.2.11-5632.2.11.7-37 KS Performance Trend Data 2.2.11-5642.2.11.7-38 RS Performance Trend Data 2.2.11-5652.2.11.7-39 Refrigeration System Secondary Loop Leakage 2.2.11-567Tracking (10 Day Averages)2.2.11.7-40 Refrigeration System Primary Loop Leakage (lO D_V 2.2.11-568

Averages )2.2.11.7-h! Refrigeration System Primary Loop Leakage (i0 Day 2.2.11-569

e Averages )2.2.11.7-42 Refrigeration System Secondary Loop Leakage (i0 2.2.11-570

D_V e Averages )2.2.11.7-43 Refrlgeration System Food Freezer Temperature Trend 2.2.11-5762.2.11.8-1 Habitation Area Pressure Control System 2.2.11-5972.2.11.8-2 Habitation Area Latching Vent Valve 1B74535-501 2.2.11-5982.2.ii.8-3 Habitation Area Solenoid Vent Valve 2.2.11-6002.2.11.8-4 Pressurization and Pressure Control System Hablta- 2.2.11-601

tlon Area No._-Propu!slve Vent2.2.11.9-I Vacuum System _chematic 2.2.11-6092.2.11.10-1 Fnetmatic Control System 2.2.11-6262.2.12.1-i Suit Drying Station 2.2.12-42.2.12.1-2 Suit Drying Perfona_:Ice CX-5 Testing (_"r in OBMS) 2.2.12-Al


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iI umber age

N P

2.2.12.2-i Suit Drying Station 2.2.12-2.2.12.2-2 PGA Support Equil,ment Stowage 2.2.12-2.2.13.2-1 SWS Equipment Stow3ge 2.2.13-2.2.13.2-2 OWS Stowage 2.2.13-2.2.13.2- 3 0WS Stowage Compartments 2.2.13-2.2.13.2-4 Tissue Dispenser - Installation 2.2.13-2.2.13.2-5 Fecal Bag Dispenser 2.2.13-2.2.13.2-6 Towel Dispenser 2.2.13-2.2.13.2-7 Trash Container 2.2.13-2.2.13.2-8 Food Boxes 2.2.13-2.2.13.2-9 Food Freezers and Food Chiller 2.2.13-2.2.13.2-10 Urine Freezer 2.2.13-2.2.13.2-11 Film Vault 2.2.13-2.2.13.2-12 Equipment Restraints - Internal 2.2.12-2.2.13.2-13 Plenum Bag 2.2.13-2.2.13.2-14 Tool and Repair Kits 2.2.13-2.2.14.1-1 Model DSV7-321 Wei6h md Balance Kit 2.2.14-2.2.14.1-2 Model DSV7-322 Forward and Aft Hoist Kit 2.2.14-2.2.14.1-3 Model DSVT-323 Stage Transporter 2.2.14-2.2.14.i-4 Model DSV7-324 Stage Cradles Kit 2.2.14-2.2.14.i-5 Model DSVT-325 Stage Handling Kit 2.2.14-2.2.14.1-6 Model DSV7-335 Handling Kit 2,2.14-2.2.14.1-7 Special Tool Kit (DSV-hB-305) 2.2.14-2.2.14.i-8 Desiccant Kit, Secondary, Saturn S-IVB (DSV-hB-365) 2.2.14-2.2.14.1-9 Beam Kit, Cover Hoist, Saturn S-IVB Stage 2.2.14-

(DSV-_B-368)2.2.1_.i-i0 Support Kit Dummy Interstage and Engine Protective 2.2.1_-(DSV-_B- 392)2.2.1_.I-ii Desiccant Kit, Static, S-IVB S_age (DSV-4B-450) 2.2.14-2.2.14.1-12 Dynamic Desiccant Trailer 2.2.14-2.2.1_.i-13 Weigh and Balance Kit, St_ (D6V-4B-345) 2.2.14-2,2,1_.2-I Solar Arrm_" Hoisting and Handlin_ Kit Model 2.2.1_-D6VT-3042.2.1_.2-2 Solar Array Hoisting and Handling Kit Model 2.2.14-DSVT-3042.2.14_2-3 Hoisting Operations 2.2.14-2.2.14.2-4 Model DSV7- 305 2.2.1 _


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Number Page2.2.14.2-5 Solar Array Hoisting and Handling Kit Model 2.2.14-30

DSV7- 3052.2.14.3-1 Plan View of Flared Aft Interstage Access Kit 2.2.14-34Model DSVT-3262.2.14.3-2 Model DSVT-326 Flared Aft Interstage Access Kit 2.2.3.4-352.2.14.3-3 Model DSV[-326 Basic Platform Assembly 2.2.14-3o2.2.14.3-4 Handling Kit Flared Aft Interstage (DSV7-hB-307) 2.2.14-372.2.14.4-1 SMMD Handling Fixture Model DSVT-345 2.2.14-472.2.14.4-2 Model DSV7-345 2.2.14-482.2.14.4-3 Model DSVT-346 LBNPD in Shipping Container 2.2.14-492.2.14.h-4 LBNPD With Hoisting Adapter installed Model 2.2.14-50

DSV7-3462.2.14.4-5 Fork Li_'t (P/O Model DSV7-349) 2.2.14-512.2.14.4-6 Model DSV7-347 Handling and Installation Kit 2.2.14-522.2.14.4-7 Model DSV7-347 Handling and Installation Kit 2.2.14-532.2.14.4-8 Control Console in Handling Fixture Model 2.2.14-55DSV7-3482.2.14.4-9 Control Console on Equipment Handling Cart Model 2.2.14-56DSVT-3482.2.14.4-10 Installation of Control Console MI31 Model 2.2.1h-57

DSV7-3482.2.14.4-11 Motor Base Handling GSE Model DSV7-348 2.2.14-582.2.14.4-12 Model DSV7-3h9 Fork Lift - Configuration A 2.2.14-592.2.14.4-13 Model DSV7-349 Fork Lift - Configuration B 2.2.14-602.2.14.4-14 Model DSVT-349 Hoisting GSE for ESS Console and 2.2 14-61

Metabolic Analyzer2.2.14.4-15 Model DSVT-349 MI71 Ergometer Handling GSE 2.2.14-622.2.14.4-16 Model DSV7-35 _.B_4D Handling GSE 2.2.14-632.2.14.4-17 BMMD Handling GSE Model DSV7-351 2.2.14-642.2.14.4-18 Right Side View of ASMU on Donning Station 2.2.14-652.2.14.4-19 Model DSV7-352 ASMU Adapter 2.2.14-662.2.14.4-20 Right Side Donning Station on ]385337-1 Cart Model 2.2.14-67DSV7-3522.2.14.4-21 Model DSVT-352 Positioning ASMU on Donning Station 2.2.14-682.2.14.4-22 Model I)_VT_'L;_Installution of Protective Ca_e 2.2.14-692.2.14.4-23 PSS Bottle Handling Hook Model DSV7-352 2.2.14-902.2.14.4-24 Model DSVT-352 988 Bottle 2.2.14-712.2.14.4-25 Model 9SV7-353 Common Flisht Stowage Contalnerl 2.2.14-73

Handlin_ C_Exxv


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Number Page

2.2.14.4-26 Model DSV7-353 AMS support 2.2.14-72.2.14.4-27 Model I_GV7-353 AMS Handling Adapter Assembly 2.2.14-752.2.14.4-28 Model DSV7-355 Exp S063 HandlinH Kit z.2.14-72.2.lb.4-29 Mo4el DSVT-355 Alignment Fixture 2.2.14-(2.2.14.4-3C Model DSV7-357 Exp S183 UV Panarama Handling 2.2.14-7and Insta/lation Kit2.2.14.4-31 Exp TO20 FCMU Hand__ing and Installation Kit ?.2.14-7

DSV7-3592.2.14.4-32 Photometer Container Handling GSE Model DSV7-361 2.2.14-82.2.14.4-33 Model DSV7-361 Photometer Handling GSE 2.2.14-82.2.14.h-34 Model DSV7-361 Sample Array Container Handling GSE 2.'_._4-2.2.14.4-35 Inverter Handling GSE DSV7-367 2.2.14-82o2.14.4-36 ETC Stowage Container Handling GSE DSV7-367 2.2.14-82.?.14.4-37 Model DSV7-367 ETC Handling GSE -.2.14-2,2.14.4-38 Model DSV7-367 ETC Support Stand 2.2.14-82.2.14.4-39 Model DSVT-372 A9 Container Handling GSE 2.2.14-82.2.14.5-1 Meteoroid Shleld Handling Kit - DSV7-302 2.2.14-92.2.14.5-2 Meteoroid Shield Handling Kit - DSV7-302 2.2.14-92.2.lb. 5-3 Meteoroid Shield Handling Fixture 2.2.14-92.2.14.5-4 Meteoroid Shield GSE Hardware for Installation 2.2.14-952.2.14.5-5 Hoist and Rigging Fixture Assembly 2.2.1_-92.2.14.5-6 Motel D6V7-371 Meteoroid Shield Counter Balance 2.2.14-9Kit2.2.14.6-i Crew Quarters Veritcal Access Kit 2.2.14-i2.2.14.6-2 Vertical Crew Quarters Access Kit Model DSV7-303 2.2.14-12.2.14.6-3 Access Platform Assembly 2.2.14-12.2.14.6-4 Access Platform to Support Rall (Rolling Position) 2.2.14-12.2.14.6-5 Access Plat_orm to Supp,rt Rail (Locked/Unlocked 2.2.14-1Position)2.2.14.6-6 Access Stands for Installation of Kit 2.2.14-12.2.14.6-7 Crev Quarters Access Kit Model DSV7-303 2.2.14-12.2.1_.6-8 Crew Quarters Floor Plates DSV7-303 2.2.14-i2.2.14.6-9 Plenum Area Access Eqtilpment 2.2.14-12.2.14.6-10 Model DSV7-307 Upper Dome Protective Cover/Access 2.2.14-1Kit


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Numbez Page2.2.14.6-13 LH2 Tank Dome Protective Cover and Access Kit Model 2.2.14-115DSVT-3072.2.1_.6-!h Lal2 Tank Dome Protective Cover and Access Kit Model 2.2.1_-I16DSV7-3072.2.14.6-15 Protective Covers 2.2.14-11 "2.2.14.6-16 Model DSVT-311 Hoist Assembly 2.2.14-ii92.2.14.6-17 Model DSVT-31i Dolly Track 2.2.1h-1202.2.14.6-18 Model DSV7-311 Food Container Handling GSE 2.2.14-].212.2.14.6-19 Model D6V7-311 Urine Return Container Handling GSE 2.2.14-1222,2.14.6-20 Model DSV7-311 Storage Container Handling GSE 2.2.14-1232.2.14.6-22 Model DSV7-311 Water Contsiner Handling GSE 2.2.14-1242.2.14.6-22 Model DSV7-311 Portable Water Tank Handling GSE 2.2.14-1252.2.14.6-23 Film Vault Drawer Handling GSE Model DSVT,-311 2.2.14-1262.2.14.6-24 Model DSV7-311 Portable Water Tank Checkout 2.2.14-127

Handling GSE2.2.14.6-25 Model DSV7-311 HSS Cart 2.2.14-1282.2.14.6-26 Cable Weight Assembly _nstallation Model DSV7-311 2.2.14-1292.2.14.6-27 Hatch Transportatica Kit Model DSV7-311 2.2.14-1302.2.14.6-28 Hatch Transportation Kit Model DSVT-317 2.2.14-1312.2.14.6-29 Handling Fixture for Access Panel Meteoroid Shield 2.2.14-132Segment,2.2.1_.6-30 Flared Af_ Interstage Access Kit Model DSVT-,326 2.2.14-1342.2.14.6-31 Plan View of Flared Aft _nterstage Access Kit Model 2.2.._4-135DSV7-3262.2.14.6-32 Model DSV7-326 Flared Aft Interstage Access Kit 2.2.14-1362,2.14.6-33 Model DSV7-326 Basic Platform Assembly 2.2.14-1372.2.14.6-34 Forward Skir_ Access Kit Model DSV7-325 2.2.14-1382.2.14.6-35 Dome Portective Cover/Access Kit and Forward Ski:'t 2.2.14-139

Access Kit2.2.14.6-36 Basic }latform Asse,,bly 2.2.14-1402.2.14.6-37 Basic Platform AAsembly with Upper Level Platform 2.2.14-Ihi2.2.14.6-38 Forward Skirt Access Kit - Access Kit Modlfication 2.2.14-1422.2.14,7-1 Model DSV7-327 Aft Umbilical Carrier 2.2.14-1482.2.14,7-2 Aft Umbilici',_]t, Checkout Stand (DSV-_B-346) 2.2.14-i492.2,14,7-3 Umbilical Kit, Forward Launcher (DSV-hB-316) 2.2,14-151(DSV7-373)2.2.1_,8-1 Vacuum Pumping Unit Installation (D6VT-314) 2.2.1_-1532.2.1_.8-2 Pluld System Schematlc (D_VT-314) 2,2.14-15'.

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Number Pa_ei --'-'--- -'----

2.2.14.8-3 Refrigeratioa Subsystem Service Unit DSVT-315 2.2.14-156= Front View (Door Removed)2.2.14.8-4 Refrigeration Subsystem, S_rvi ce Unit 2.2.14-1572.2.14.8-5 A...cessoryKit Mechanical Test (DSV7-316) 2.2.14-1%;2.2.14.8-6 Accessory Kit - Mechanical Test (DSV7-316) 2.2.14-16_

Pressure Dec_7 Leak Detector Schematic2.2.14.8-7 Accessory Kit Mechanical Test (DSVT-316) 2.2.i,-16 2.2.14.8-8 Air Content Tester Assembly P/N IB87918-I 2.2.14-163

' (DSV7-316)2.2.14.8-9 Accessory Kit Mechanical Test (DSV7-316) 2.2.14-1642.2.14.8-10 Flexible Hose End Fitting GSE - RS Coolanol-15 2.2.14-170

; 2.2.14.9-I Ground Thermal Conditioning System DSV7-301 2.2.1_-1752.2.14.9--2 Ground Thermal Conditioning System - System 2.2.14-176, Configuration D6V7-3012.2.14.9-3 Ground Thermal Conditioning System DSVT-301KSC 2.2 14-177Operational Configuration2.2.14.9-4 Ground _ermal Conditioning System DSVT-301 CCU 2.2. I_-178

Mechanical S_hematic2.2.14.9-5 TCU Temperature vs. Flowrate 2.2.14-1812.2.14.10-1 Ground Thermal Conditioning System DSV7-334 2.2.14-1882.2,14.10-2 Ground Thermal Conditioning System DSV7-334 2.2.1_-1892.2.14.10-3 Ground Thermal Conditioning System DSV7-334 2.2.14-1902.2.14.10-4 Ground Therm_ Cc_ditionlng System OWS Interior 2.2.14-191D6V7-3342.2.14.11-1 Distribution System, Environmental Control Kit 2.2.14-197(DSVT-3hh)2.2.14.11-2 Normal OperatlQnal System, VAB (& Fad Contingency) 2.2.14-19_DSV7-3_h2.2.1_.12-i Accessory Kit Mechanical Test (DarT-316) 2.2.1_-2012.2.14.12-2 Accessory Kit - Mechanical Test (DSV7-316) 2.2.14-202Scientific Airlock Leak Test Kit Schematic2.2.14.13-i HSS Water Subsystem Checkout and Sterilization 2.2.1_-207

Console DSV7-3122.2.14.13-2 0WS Checkout and Steril._zatlon Wa_er Subsystem, 2.2.1_-208Hss (DeVT-_2)2.2.14.13-3 OWS Checkout and Ste,'illzation Water Subsystem, 2.2.14-209HSS (_V7-_2)2.2.14.13-h Water Subsystem GSE D6V7-312 2.2.1_-2102.2.1b.14-i Checkout Kit, W_te Menagement System (DSV7-373) 2.2.14-_I>2.2.1_.14-2 Ground Support Equipment - Waste Management - 2.2.11,-_1,Fecal/Urine Collector Air Distribution Te_t

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i Number Page2.3.2-16 Refrigeration System Component-to-Bos_ Fluid 2.3-56Connection2.3.2-17 Refrigeration System Flare Tube Connector (MC) 2.3-58F?

! 2.3.2-18 Refrigeration Subsystem - Refrigeration Pump Unit 2.3-59Enclosure2.3.2-19 Shrouded Coolant Combustibility Test-A1 Tape Intact 2.3-612.3.2-20 Shrouded Coolant Line Combustibility Test Sample - 2.3-62

A1 Tape Removed2.3.2-21 Shrouded Coolant Line Combustibility Test Sample - 2.3-63

A1 Tape Removed2.3.2-22 Shrouded Coolant Combustibility Test - A1 Tape 2.3-64Intact2.3.5.1-1 Allowable Surface Area of High Vapor Pressure 2.3-90

Materials2.3.5.1-2 S-13G Thermal Control Coating Test Results 2.3-922.3.5.1-3 S-13G Paint Predicted Outgassing Rate as a Function 2.3-93of Time in Orbit2.3.5.1-h 0WS External Coatings 2.3-9h3.1-1 Reliability and Safety Inter-relations Between 3-3Functions and Activities3.2.2-1 Design Review Flow Chart 3-175.5-1 OWS-1 Post Manufacturing Checkout Schedule 5-60

(Page 1 of 2)5.5-1 OWS-I Post Manufacturing Checkout Schedule 5-61

(Page 2 of 2)5.6.1-1 Spacecraft Overall Schedule - Sky!ao 1 5-886.1.i-i Memorandum - Orbital Workshop Configuration 6-2Definition6.1.2-1 Skylab - OWS Change Request Form 6-47.2-1 MDAC-W/HOSC Coordination Interfaces 7-57.2-2 HOSC Skylab Operations Support Facility Layout 7-77.2-3 Skylab Data Flow 7-117.2-4 Action Request Flow 7-177.3.2-1 Orbital Workshop Prelaunch and Mission Support Team 7-207.3.2-2 OWS Mission Support 7-217.3.b-I Overall Action Item Flow 7-2_7.3.6-i OWS Mission Support Center Location and General 7-32

Layout8.1.2-i Orbital Workshop Solar Arra_ System 8-10

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i Number Page8.i.2-2 Refrigeration System 8-128.1.2-3 Film Vault Packaging 8-138.1.2-_ Thruster Attitude Control System 8-158.1.2-5 OWS Environmental Control System 8-168.1.2-6 Skylab Personal Hygiene System 8-188.1.2.7 Water System 8-198.1.2-8 Waste Management System 8-208.1.2-W Waste Collector and Processors 8-23


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i PR/_C_)/NG PAO_ BLANK NOT FILMED

: T_LF, S

Number Page1.2.2.5-1 Skylab Missions - Calendar Day/Day of Year/Mission 1-14

Day1.2.2.5-2 0WS Experiment Activity 1-162.2.1.2-1 Orbital Workshop Internal Color Requirements 2.2.1-292.2.1.3-1 TC-9 Qualification Test: TACS Sphere Installation 2.2.1-1582.2.1.3-2 TACS Nitrogen Gas Storage Spheres Production 22.1-161

Acceptance Test2.2.1.4-1 Aft Interstage - Design Ultimate Loads 2.2.1-1792.2.1.5-1 SL-1 Orbital Workshop Module Wieght Growth 2.2.1-1882.2.2.1-1 Meteoroid Shield Test Verification Summary 2.2.2-252.2.2.1-2 Problem Summary Subsystem Habitation Area Tank - 2.2.2-32Meteoroid Shield2.2.2.2-1 Meteoroid Protection Test Verification Su_amary 2.2.2-472.2.2.2-2 Meteoroid Proection Structural Evaluation Summary 2.2.2-502.2.3-1 Thermal Control System Performance Summary 2.2.3-52.2.3-2 A/M Cooling to 0WS 2.2.3-152.2.3-3 Environmental/Thermal Control Subsystem Design 2.2.3-19Parameters2.2.3-4 Convective Heater Design Parameters 2.2.3-392.2.3-5 Radient Heater Design Requirements 2.2.3-h32.2.3-6 HPI Design Parameters 2.2.3-622.2.3-7 Orbital WorLshop Optical Coatings 2.2.3-682.2.3-8 Heat Pipe Design Parameters 2.2.3-812.2.3-9 OWS Thermal Control System Optical Properties 2.2.3-95

Requirements Verification2.2.3-10 Average Flow Velocities Test Data 2.2.3-1042.2.3-11 SL-2 Ventilation Duct Flow Summary 2.2.3-1i72.2.3-12 SL-3 Ventilation Duct Flow Summary 2.2.3-1202.2.3-13 Gold Tape Optical Properties 2.2.3-1502.2.3-1h Common Bulkhead Heat Leak 2.2.3-152


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Number Page

2.2.3-15 OWS Electrical Heat Removal Capability 2.2.3-190

i 2.2.3-16 Temperature Instrumentation Error Summary 2.2.3-195.2.6.3-1 Qualification Test Summary 2.2.6-302.2.7.2-1 Illumination System Components 2.2.7-62.2.7. h-i lll_Amination System - OWS - Usage 2.2.7-312.2.8.1-1 Huntington Beach Post Manufacturing Test Affecting 2.2.8-10

OWS Commthnication System2.2.8.2-1 Huntington Beach Post Manufacturing Tests Affecting 2.2.8-32

OWS DAS Subsystem2.2.8.2-2 KSC Testing of the DAS Subsystem 2.2.8-332.2.8.2-3 Significant DAS Qualification Test Problems 2.2.8-342.2.8.2-4 Significant Huntington Beach DAS System Test 2.2.8-35Problems2.2.8.2-5 Significant KSC DAS Subsystem Test Problems 2.2.8-362.2.8. h-1 Huntington Beach Post Manufacturing Tests Affecting 2.2.8-77

OWS TV System2.2.8.4-2 KSC Testing of the TV System 2.2.8-792.2.9.2-1 Caution and Warning Subsystem Panel Displays 2.2.9-102.2.10.1-1 OWS Experiments 2.2.10-22.2.10.1-2 Experiment - Related ICD's 2.2.10-42.2.10.1-3 0WS Experiment Accommodations Requirements Summary 2.2.10-72.2.10.1-h Receiving Inspection Summary 2.2.10-232.2.10.1-5 VCL Experiment Test Summary 2.2.10-252.2.10.1-6 KSC Test Procedures Applicable to Experiment 2.2.10-26Accommodations2.2.10.1-7 Skylab Experiment Accomplishment Summary 2.2.10-282.2.10.h-i Astronaut - Induced Limit Loads on SAL 2_2.10-492.2.10.5-1 Random and Sinusoidal Vibration Load Factors 2.2.10-68

(Limit) at Liftoff and Boost2.2.11.1-1 Waste Management Subsystem Development Tests 2.2.11-1002.2.11.1-2 Waste Mana6ement Subsystem Qualification Tests 2.2.11-1012.2.11.1-3 Waste Manasement System Test Assessment Document 2.2.11-102Index2.2.11.1-4 Problem Summary, Collection Module 2.2.11-1052.2.11.1-5 Problem Summary, Centrifugal Urine Separator 2.2.11-106

Assembly (CUSA)2.2.11.1-6 Problem Summary Vacuum Cleaner and Power Module 2.2,11-1072.2.11.1-7 Problem Summary, Waste Processor 2,2.11-108


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Number Page2.2.ii.1-8 Problem Summary, Waste Tank - Trash Disposal 2.2.11-ii0Airlock2.2.ii.1-9 Trash Disposal Structural Evaluation Summary 2.2.11-1232.2.11.1-10 Daily Urine Volume (LI Analysis) - First Mission 2.2.11-16_2.2.11.1-ii Daily Urine Volume (II Analysis) - Second Mission 2.2.11-16'{2.2.11.i-12 Daily Urine Volume (LI Analysis) - Third Mission 2,2.11-1692.2.ii.2-1 Wa.ter Budget 2.2.11-2002.2.11.2-2 Water System Development and Qualification Test 2.2.11-27hLine Stems2.2.11.2-3 Water System Items in Test and Assessment Document 2.2.11-275

(TAD) MDC G047hC2.2.11.2-h OWS Water Subsystem Problem Summary 2.2.11-2762.2.11.2-5 Water Syst-m Development and Qualification Test 2.2.11-282

Completion Statements2.2.11.2-6 Tank 1 Potable W___r Analysis Prior to Launch, 2.2.11-328DOY 06__2.2.11.2-7 T-u}; 1 Potable Water Analysis Prior to Launch, 2.2.11-329

DOY 0962.2.11.2-8 Tank lO rotable Water Analysis Prior to Launch, 2.2.11-330

DOY 0712.2.11.2-9 Tank l0 Potable Water Analysis Prior to Launch, 2.2.11-331

DOY 0962.2.11.2-10 Tank 2 Potable Water Analysis Prior to Launch, 2.2.11-332DOY 0652.2.11.2-11 Tank 2 Potable Water Analysis Prior to Launch, 2.2.11-333DOY 0962.2.11.2-12 Tank 3 Potable Water Analysis Prior to Launch, 2.2.11-334DOY 0682.2.11.2-13 Tank 3 Potable Water Analysis Prior to Launch, 2.2.11-335

DOY 0962.2.11.2-ih Tank h Potable Water Analysis Prior to Launch, 2.2.11-336DOY 0672.2.11.2-15 Tank 4 Potable Water Analysis Prior to Launch, 2.2.11-337

DOY 0962.2.11.2-16 Tank 5 potable Water Analysis Prior to Launch, 2.2.11-338

DOY 0692.2.11,2-17 Tank 5 Potable Water Analysis Prior to Launch, 2.2.11-339

DOY 0962.2.11.2-18 Tank I Potable Water SL-I/SL-2 Data from Sample 2.2.11-3h0Returned from Orbit2.2.11.2-19 Tank 2 Fotable Water SL-3 Data fro_ Sample Returned 2.2.11-3_i' from Orbit

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Number Page2.2.11.2-20 Potable Water - SL-4 Data from Samples Returned 2.2.11-342from Orbit2.2.11.2-21 OWS Action Summa_-y - System: Water-Mission: SL-2 2.2.11-3502.2.11.2-22 OWS Action Summary - System: Water-Mission: SL-3 2.2.].1-352.2.11.2-23 OWS Action Summary - System: Water-Mission: SL-h 2.2.11-3522.2.11.4-i Test Summary Sheet - OWS Whole Body Shower Water 2.2.11-418

Bottle Module Assembly2.2.ii. 7-1 Refrigeration System Design Requirements 2.2.11-4662.2.ii. 7-2 ICD 13M20926 Food Storage Requirements 2.2.11-4682.2.11.i-3 Major Design Parameters 2.2.11-4692.2.11.7-4 Refrigeration System Development and Qualification 2.2.11-497

Test Line Items2.2.ii.7-5 Refrigeration Subsystem Test Problem Summary 2.2.11-5002.2.11.7-6 Refrigeration System Items (TAD) Test and 2.2.11-509

Assessment Document MDC G0674C2.2.11.7-7 Refrigeration System Performance Summary - Primary 2.2.11-554

Loop2.2.11.7-8 RS Action Items - SL-I and SL-2 2.2.11.5812.2.11.7-9 RS Action Items - SL-3 2.2.11-5852.2.14.1-1 Spacecraft Handling and Transportation Equipment 2.2.14-2

Safety Factors2.2.14.2-1 SAS Handling and Transportation Equipment Safety 2.2.14-24Factors2.2.14.3-1 Interstage Handling and Transportation Equipment 2.2.14-33

Safety Factors2.2.14.4-i Experiment Handling Equipment 2.2.14-402.2.14.5-1 Meteoroid Shiel_ Handling and Installation 2.2.14-91

Equipment Factors of Safety2.2.14.6-1 Access Kits Factors of Safety 2.2.14-1002.2.14.7-1 Umbilicals Handling Equipment Factors of Safety 2.2.14-146_.3,2-i MDAC Contractual References, Responsibilities, and 2.3-5

Reporting Tasks2.3.2-2 Suppler Contractual References, Responsibili_ie , 2.3-6

and Reporting Tuks2.3.2-3 Materials U.ed 2.3-82.3.2-4 Tabulation of Significant Flammable Materials 2.3-112.3.2-5 Stowage Concepts 2.3-222.3.2-,6 Component and System Tests 2.3-_6


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t

I Number Page2.3.5. i-I Materials Outgassing Requirements, Design Criteria 2.3-89and Definitions2.3.5.1-2 External Materials Review - Acceptable per 2.3-9550M02442 "V"2,3.5.1-3 External Materials Review - Acceptable per CEI 2.3-96

Specification2.3.5.1-4 External Materials Review Rationale for Use 2.3-993.2-1 Reliability Program Functions by Development Phase 3-43.2-2 Criticality Categories 3-54.i-i Key Elements of the 0WS System Safety Program 4-34.2.3.1-1 Review of Operations with Potential for Damage to 4-21

Equipment or Injury to Personnel4.2.3.1-2 Special Safety Reviews h-244.2.3.2-1 Safety and Safety Related Audits 4-256.2.2.2-1 CDR Approved Design Baseline 6-207.3.5-1 0WS Mission Support Action Item Summary - Number 7-27

of Actions by OWS System vs. Mission Period7.3.5-2 0WS Mission Support Action Item Summary - Number 7-28

of Action Items by Initiating Agency vs. MissionPeriod7.3.5-3 OWS Mission Support Action Item Summary - Number 7-29

of Action Items by 0WS system vs. Type of ActionItem

7.3.7-1 SL-I Manning 7-397.3.7-2 SL-2, SL-3, SL-4 Activation/Deactlvation Manning 7-407.3.7-3 Normal Orbital Operations MSR Minimum Manning 7-418.1.1-1 New Technology Patent Disclosures Developed Under 8-2

NASA Contract NAS9-6555 Orbital Workshop9.2.3-1 OWS Reviews 9-329.2.3-2 Cluster Revie'_s 9-33


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ABBREVIATIONS AND ACRONYMS

A Ang s t romsAC Alternating CurrentACE Acceptance Checkout EquipmentACQSS Acquisition Sun SensorACS Attitude Control SystemADP Acceptance Data PackageALSA Astronaut Llfe Support AssemblyAM Alrlock ModuleAPCS Attitude & Pointing Control SystemARC _=es Research Center

' ASAP Auxiliary Storage and PlaybackATM Apollo Telescope Mount: ATMDC Apollo Telescope Mount Digltal ComputerBTU British Thermal UnitsCBRM Charger Battery Regulator Modulei CCB Change Control BoardCCOlt Combined Contaminants, Oxygen, Humidity

i CCS Command Communication SystemC&D Control and DisplayCEI Contract End ItemCFE Contractor Furnished EquipmentCG Center of GravityCL CenterlineCluster SWS plus CSM (used synonymously wi_.h "Orbital Assembly")CM Con=and ModuleCMG Control Moment GyroCMGS/TACS Control Moment Gyros Subsystem/Thruster Attitude Control

SubsystemC/O CheckoutCOAS Crew Optical Alignment SightCO2 Carbon DioxideCOFW Certificate of Flight WorthinessCOQ Certificate of Qualificationcpe cycles per secondCRS Cluster Requireunt8 SpecificationCSM C_and Service ModuleC&W Caution and WarningDA Deployment Assemblydb Decibeldc Direct CurrentDCS Digital Command SystemDCSU Digital Computer Switching UnitDDA Drawing Departure AuthorisationDDAS Digital Data Address Systemdng. DegroeDTCS Digitai Test Command SystemDTMS Digital Test Measuring System

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3

ECP Engineering Change ProposalECS Environmental Control SystemEMC Electrcenagnetic CompatibilityEMI Electromagnetic InterferenceEPCS Experiment Pointing Control SubsystemEPS Electrical Power SystemERD Experiment Requirement DocumentE$E Electrical Support EquipmentESS Experiment Support SystemETR Eastern Test RangeEVA Extravehicular Activity*F Degrees FarenheitFAg Fixed Alrlock Shroudfc foot candlesFM Frequency Modulationfps feet per secondFSS Fine Sun Sensorft. Feetg Acceleration due to Earth's GravityGFE Government Furnished EquipmentGrms G Level, root mean squareGSE Ground Support EquipmentH20 Waterlie HeliumHSS Habitability Support SystemHz HertzICD Interface Control DocumentIOP In Orbit PlaneIU Instrumentation UnitIU/TACS Instrument Unit/Thruster Attitude Control SubsystemIVA Inert-Vehicular ActivityJSC Johnson Spacecraft CenterKHz KilohertzKSC Kennedy Spaceflight CenterLCC Launch Control CenterLCG Liquid Cooled GarmentLH2 Liquid Hydrogen10 2 Liquid OxygenLRC Langley Research CenterLV Launch VehicleLVDC Launch Vehicle Digital ComputerNDA Multiple Docking Adapter14GSK Maintenance _round Support Equipment14148 Megahertzt4RD Mission Requirements Docu_ntMS Margin of Safetym/set. MillisecondMSFC Marshall Space Flight CenterMSFt4 Manned Space Flight NetvorkMSOB Manned Spacecraft Operations Building


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N2 NitrogenNASA National Aeronautics and Space AdministrationNHB NASAHandbookNICd Nickel CadmiumNM Nautical Miles02 OxygenOA Orbital Assembly (SWS and CSM - Used synonymously wlth"Cluster")OWS Orbital WorkshopAP Differential PressurePCH Pulse Code ModulationPCS Pointing Control SystemPNC Post Manufacturing CheckoutPOD Planning Operational Dosepsi pounds per square inchpals pounds per square inch absolutepsld pounds per square inch differentialq HeatRCS Reaction Control SystemRF Radio FrequencyS-ib First Stage of Saturn I-B Launch VehicleS-II Saturn IISAL Scientific Air LockSAS Solar Array SystemSCH Speclficacion Change NoticeSL Skylab ProgramSM Service ModuleSWS Saturn Workshop (PS/HDA/ATM/IO_/OWS/IU/ATMDeploymentAssembly)AT Differential TemperatureTACS Thruster Attitude Control SystemTCP.D Test and Checkout Requirements DocumentTCSCD Test and Checkout SpeclflcaClon and Criteria DocumentUV Ultra VioletVAB Vehicle Assembly Building (HI-Bay)Vdc VoIte direct currentVIIF Very High FrequencyWHS Waste _tanasement SystemWSS Water SubeystnZ-LV(E) Z Axis in Local Vertical (Earth Resources Attitude Mode)Z-LV(R) Z axis in Local Vertical (Rendezvous Attitude Mode)

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2.2.11 Habitability Support Systems

2.2.11.1 Waste Management Subsystem

A. Design Requirements - The Waste Management Subsystem (WMS) shallprovide for the collection, processing, storage, and/or disposalof the feces, urine, and vomltus as well as debris, particulatematter, and free water from the atmosphere, and shall providesupport for experiments M071 (Mineral Balance), and M074 andM073 (Bi-Assay of Body Fluids). It shall also provide a WasteDisposal System utilizing the LOX tank as a waste tank for dis-posing of all wet and dry materials and refuge collected in thehabitable ar_.asinteE_al to the oroltal assembly.

l/ General Requirements - The WMS _hall be capable of collectingurine, feces, and vomit simult_,eousl>; shall be designed topreclude mixing and cross contamination of urine, feces,

vomit, and debris between crew members; and shall preventcross contamination in excess of one percent between thesamples from the same crew member obtained on different days.The WMS shall provide the capability for transferring pro-cessed and identified samples of the collected urine, feces,and vomit to the Command Module (CM) for subsequent return toearth for analysis. All atmosphere used in the collectionprocess of the WMS equipment (except for intentionally dumpedatmosphere) shall be passed through a replaceable odor con-trol filter. Odor removal assemblies, with filter replace-menta as required, shall maintain the level of malodorousconstituents of flatus within the compartment as specifiedin paragraph 3.3.1.2.1.7 of CP2OSOJIC. It shall _lso


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provide for the collecton, temporary storage and disposalinto the waste tank of refuse collected in the habitable

areas of the workshop. The functions, equipment, items andgeneral requirements for the _4S are listed below:

Fecal collection: vacuum drying and storage Urine collection: sampling, volume determination,

dis_os_.l and/or freezing, and storage of samples Vomitus collection: vacuum drying and storage Debris collection: deactivation and storage Removal of free water from the atmosphere Storage of new and used tissues, empty and filled

collection venicles

Sample processing and storage techniques, which arecompatible with mission operations, from launch throughrecovery.

Collection, temporary storage and disposal of refuse

Equipment Items : Fecal collector Urine collector Vomitus containers Vacuum cleaner Waste processor Urine freezer Ccllection bags Storage containers Toilet tissues and dispenser Urine return container

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Disposal bags 'iTasnAirlock

General Requirements : All subsystems shall be def _ned to _u;port a cre_ of

three for each misslo_ All equipment provided for personal use of the crew

shall be id.ntified for each crew member. Aids and restraints shall be provided as necessary for

the operation of each of the subsystems. One-handedoperation shall be a design goal

All materials used in the subsystem shall be selectedto minim_ze particulate contamination.

The subsystem shall be designed to provide the capa-bility of bei:_ cleaned for collections o_'accumulateddebris or spilled debris

TEe subsystems shall _e designed to minimize equipmenthandling and operations

All systems necessary for life suppo'_ are to besupplemented by contingency methods in the event offailure. These backup efforts nee_ not support theexperiment requirements

The s_bsystem shall provide for tanitLry disposal ofwaste which is no_ to be returned for analysis, suchas soiled ragss toveZs clothin_, waste water and refuse.

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a. Fecal Collector Requirements - The fecal collector shallprovide the capability to collect and contain all con-

: sistencies of fecal matter. The requirements for thecollector are:1. The fecal collector shall provide a p_sitlve means

to ensure separation, collection, and containmentof the feces and wiping material.

2. Capability shall be provided to clean the fecalcollector seat and associated equipment after use.

3. A fixed receptacle shall be provided to support thefecal collector bags during use.

h. The fecal collector seat and the related restraintequipment shall be arranged in such a manner that

! the crewman may assume the squat position duringdefecation and be able to perform the wiping with-

out escape of the feces from the collectioncontainer.

5. The opening of the fecal collector seat shall bedesigned to minimize the possibility of smearing

I the seat with residual fecal material by relativemotion between the buttocks and the fecal collectorseat.

6. All equipment, controls, and displays of the WMSshall be visible and accessible to the astronautwhile positioned on the fecal collector seat.

7. The fecal collection process shall not alter theconstituents of the fecal material (including water)


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until a mass measurement has been performed andits results recorded. After the mass measurement,the fecal collection shall be vacuum dried.

_. The maximum duration of each complete defecationcycle (excluding defecation) shall not exceed 15minutes. The cycle shall include system prepara-tion, initiation of processing, and preparation ofthe WMS for the next cycle. The WMS shall bedesigned to limit initial preparation time to nomore than 30 seconds.

9. The clear depth measured from the top of the fecalcollector seat to the bottom of the fecal collec-tion bags shall be a minimum of thirteen inches.

i0. Accommodations shall be provided for an articu-lating GFP mirror near the fecal collector.

b. Urine Collector Requirements - The urine collectorshall provide the capability to collect, contain,determine volume, sample urine, and to dispose ofexcess urine. The requirements for the urine collectorare:1. The urine receiver shall completely enclose the

urine stream during the collection process. _etailoff or dripping portion of the normal urinationprocess shall be accommodated by the urinecollector.

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f

2. The urine receiver and the urine collection unitshall be operable while the astronaut is restrainedin the seated or standing position.

3. The urine collection unit shall be designed to

i collect and contain the urine for the followingconditions :6 Average output of 2000 ml/man/24 hours

; Maximum output of 4000 mllman/24 hoursL Miniatureoutput of 600 ml/man/2h hours Maximum delivery rate shall correspond to the

_ curve shown in Figure 2.2.11. i-i.! Average of i0 micturitions/man/2h hoursi Minimum single void of 35 mlI h. A means shall be provided to control bacteria! growth, odors and contamination.

i 5. The urine collector shall provide the capabilityto extract representative samples of 122 ml

I (minimum), from a homogenous pool for freezing.The samples shall be frozen below -2.5F (-19,2C)within 8 hours of each 24 hour pool period.

6. Urine remaining after sample extraction shall bedisposed of into the LOX tank. The system shallprovide the capability to dispose of the urine atacheduled intervals.

7, The _ine collection unit shall determine thevolume of each 2h hour void to an accuracy of+ 15 percent.

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8. The urine collector shall be designed to prevent

cross-contamination between the users. A flushingcapability shall be provided as a mean, of con-trolling cross-contamination between the 2h hourpooled urine collections for each user. Theflushing system shall be capable of dispensingwater from a pre-installed water container in fouA-increments of 50 + 5 ml per crewman per 2_ hourpooling period. Use of the flushing system shalllimit the day to day cross-contamination between

I urine samples to less than one percent of thevolume collected each day. The total urine/flushresidual carry-over from day to day shall not

. exceed i0 ml.9. The 24 hour urine pool shall be maintained at a

temperature below 59F (15C). The temperature of

the pool shall not exceed 59F (15C) for more thanan accumulated time of 3 hours during the 24 hour period

lO. The maximum time for each urination cycle(excluding urination) shall not exceed one (1)minute, The cycle includes system preparation andpreparation of the WMS for the next,urinationcycle. The WMS _hall be designed to limit initialpreparation time to no more than 30 seconds.

ll. Volume measurement, sampling, sample stowage, and

zystem preparation for the next 2_ hour cy_le

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!

(excluding the actual dumping time required todispose the excess urine at scheduled intervals)shall not exceed 20 minutes total time for threecrewmen.

12. The urine collection system shall interface withthe CM for transferring, collecting, measuring andsampling, and the dumping of the urine collectedduring CM operations prior to 0WS activation.

13. A lithium chloride tracer shall be incorporated asthe prime method to determine the volume of urinecollected in each 24 hour urine pooling period.Lithium shall be added in the amount of 30 _ 0.3 mginto each pooling bag prior to flight.

14. An alternate urine collection system shall utilizeApollo type roll-on cuffs and adapters to accommo-date urine collection directly into urine collec-tion bags without the use of air entrainment.Provision shall be made on each adapter to preventbackflow. After each void, the urine collectionbags will be stowed employing the chilling pro-visions of the urine collector. Primary volumemeasurement shall be accomplished by using a lith-ium chloride tracer. The on board mechanicalvolume measuremer system shall be used. The con-tingency urine collection system shall also pro-vide the capability for extracting urine samples.

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c. Vomitus Collection - Contingency fecal bags shall beprovided to collect and contain vomitus material from

the crewmen. Specific requirements for collecting andcontaining vomit are:i. Vomitus shall not be collected in the same con-

tainer with other wastes.2. The bags shall have the capability of being

carried by the crewmen without interfering withtheir mobility and performance,

3. The bags shall be capable of operation without theaid of a vacuum source or atmosphere circulationequipment and shall be portable.

_. Each bag shall be designed to contain a minimum oflO0 ml of vomitus.The bags shall interface with the waste processorfor processing and shall interface with the GFPSpecimen Mass Measuring Device (SMMD).

6. The bags shall be provided as specified inI-SL-008.

d. Waste Processor Bmquirements - The waste processor shallprovide for vacuum-drying the fecal and vomitus collec-tions and debris collections (if necessary) so that the

waste products therein are deactivated and bacterialcontamination is prevented. Requirements for wasteprocessing are:1. All fecal and vomitus collections shall be vacuum

dried.

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2. Each processor shall have the capability of beingindividually controlled and shall include a displayto indicat_ to the Astronaut when each specimen hasbeen deactivated and is ready for storage.

3. The atmosphere overboard-leakage rste of the pro-cessor shall be apportioned from the five poundmass/day total OW8 leakage rate.

4. All control parameters necessary to monitor opera-tion of the processor shall be apparent to theoperator.

5. Six processors shall be provided.6. Temperature sensors shall provide direct power

interrupt to the heaters in the event of an over-temperature processing condition.

e. Thermal Conditioning Requirements - Provision shall bemade to freeze the urine samples to below +27F (-2.8C)within 3 hours, to OF (-17.8C) within 6 hours and tobelow -2.5F (-19.2C) within 8 hours.

f. Urine Return Requirements - Provisions shall be providedfor transferring the frozen urine samples from the OWSto Earth via the Command Module (CM). The provisionsshall have a thermal con'_rolcapability to maintain theurine samples after removal from the urine fremzer attemperstures not to exceed 17OF (-8.3C) for '_c_ours.

g. Collection Bags - Collection bags shall be provided forthe daily collection of urine, sampling of urine, and

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collection of feces. The requirement_ for the fecaland urine collection bags are:I. The fecal bags shall be fabricated from an

impermeable outer material and shall be designedfor compatible operation with the fecal collectorand the waste processor. The fecal bags shallinterfa,;e with the SMMD (GFP).

2. The urine collection bags shall be compatible withthe urine collector for 2h hour urine pooling,urine chilling, volume measurement of the urine,and transfer of the urine to the urine sample bags.The urine _'ollection bags shall also be compatiblevlth urine dumping into the waste tank or with dis-posal of f_[l urine bags into the trash airlock.

3. The urine sample bags slm_l be compatible withfreezing a m[nin_lumof 122 ml of urine and shall bedesigned for miuimum stowage volume.

h. Modified ecal bags shall be provided for use inthe CM, These bags shall be compatible with thewaste processor and shall interface with the SMMD.

5. The collection bags shall be designed to preventsplashing during waste collection. The bags shallbe configured s_ that no ccntact with the interiorsurface is required in order to seal, process, andstore the bags for return.

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6. A means shall be provided to pass gas from thecollection bags but not solids and liquids. Thebags shall be impervious to liquids, gases, andsolids when sealed.

7. All collection bags which are placed on the SMMDshall be marked with the empty bag weight to within+3.0 grams.

8. Each urine sample bag and the fecal and vomituscollection bags shall provide for recording: Designation of the Astronaut providing the

sample Time at initiation of processing or freezing Volume or mass of the sample

9. The collection bags shall be designed to requirem_nimum stowage volume. Fefer to the Stowage Listfor the quantities of bags required.

i0. The OWS waste collection bags shall interface withthe CM stowage facilities.

ii. The fecal bag shall be designed to eliminate fecalmatter from contacting the seal lip duringdefecation.

12. Urine half sample bags having a minimum volume of50 ml, shall be provided and ahall be compatiblewith the blood sample collection system.._

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h. Waste Storage Requirements - Provisions for the storageof the waste management supplies and processed samplesshall meet the following requirements:i. All supplies for sanitary operation of the WMS

shall be located in appropriate storage containers,within easy reach of an astronaut while positionedon the fecal collector seat.

2. Storace containers shall house the tissues andclean waste collection vehicles to be used forfecal, urine, vomitus, and debris collection.

B. Storage containers shall be provided for used wastecollection vehicles and the processed contents ofeach.

_. The vehicle storage containers for feces, urine, andvomitus shall be removable from the OWS Waste Manage-ment Compartment (WMC) in modular form for transferto the Apollo CM and subsequent return to earth.

i. Toilet Tissue Requirements

i. Toilet tissues and a dispenser shall be provided' for use in the WMC.2. A dispenser for the toi2et tissue shall be easily

accessible to an astronaut positioned on the fecalcollector seat.

3. The chemical composition of the toilet tissues

shall not alter the collected sample constituents.J. Vacuum Cleaner -A portable vacuum cleaner system shall

be provided to collect and contain particulate material

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from any location within the OWS. The requirements fordebris collection and cortainment are:i. Tb._portable vacuum cleaner _ygtem shall be capable

of collecting debris (including free water) andparticulate matter from the atmosphere from allaccessible areas of the OWS. After being filtered,the atmosphere shall be returned to the OWS.

2. The vacuum cleaner shall be capable of being oper-ated throughout the OWS.

3. Removable collection vehicles shall be utilized.h. The portable vacuum cleaner system shall be elec-

trically powered utilizing a universal electricalcable and preinstalled electrical Junction boxes.

5. Capability shall be provided for cleaning inrestricted areas.

6. Means shall be provided to deactiv%ge collecteddebris such as food wastes.

7. Vacuum cleaner bags shall be supplied el,specifiedin I-SL-O08.

8. The vacuum cleaner shaJl have an interlock to pre-vent operation unless a bag Is installed.

9. The vacuum cleaner shall provide the capability tocontain collected waste when the blower is notoperating. The vacuum cleaner shall incorporateprovia one to permit one-handed carrying of thevacuum cleaner and attachments and include a capa-bility to be attached to the grid floor.

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i0. The vacuum cleaner shall have opposing, non-propulsive, exhaust vents and shall have a three-

position switch for on, off, and momentary.k. Trash Collection Bags

i. La_'ge Trash Bag Shall have capability of closing and

reopening during loading and unloading oftrash items.

Shall have capability of being restrained toOWS wall locations and crewman's utility beltby means of snaps.

Opening shall be sized and designed to accom-modate all trash items defined by Logistics.

Large bag shall restrain moist and dry solids. Shall not open or rupture when exposed to

trash airlock depressurization and waste tankpressures.

, Venting shall be done through the bag material

and seams stitching. Restraint tabs shall be provided to restrain

and position bag in trash airlock.2. General Purpose (GP) Trash Bags

Loading of trash items in GP bag shall bedone by crewman using one hand.

Removing and replacing GP bag from lockerdoor shall be done w_th minimum effort tocrewman, and requiring no tools.

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'['rashitems sh_ll remain in GP b_g when trash

lid is opeL, by _ome means of restrair_t. Opening shall be sized ar.d design_ to accommo-

date all trash _tem_ defined by Logistics,

except for urine and iL_-inch (O.h06 meter,_)food ont ainers.

Shall restrain moist and dry solids.Opertlng of filled bag shall have the capabil-ity oC b_ing (:losed prior to storage in was'-_tank.

Shall not open or rupture when exposed totrash airlock depressurization, and wastetank pressures.

Venting shall be done th_'ough the bag materipland seams stitching.

Restraint tabs shall be proviaed to restrainand position bag in trash airlock.

1. Trash Airlock -The trash _irlock shall be des_:%ed toperfor_n normally in the '3psi (3_.5 kN/m _) environm_n ",

provided in the OWS. Its life shall be based on fiveoperations per da_, for lhO drays at OWS interlor ambienttemperatures. Its proof pressure shAi _.be approxlmatolyi0 pSl (68.9 kN/m 2) differential e,d shall be capableof withstanding an orbltal m_lZ'umction differential

pressure of 26 _|Id (179.3 kN/m 2) without d_ma_e (s_eFigure 2.2.11.1-2).

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In debris collection the crewman removes a debris bag from itsstowage container and installs the bag in the vacuum cleanercarmister. The debris is then collected and contained in the bagin a normal vacuum cleaning manner. The crewman then removesthe debris bag from the vacuum cleaner, seals the bag and placesit in a trash bag for eventual disposal in the waste tank by wayof the trash airlock.

In urine collection the individual crewman removes the urinereceiver from t:le drawer and installs it on the collection module.The crewman then micturates into the inlet line of the collection

module. Entrained air flow carries the urine to the centrifugalseparator; where air and urine are separated and the urinepumped into the urine bag. The urine is collected in this mannerfor a 24-hour period, and the urine bag is replaced at 24-hourintervals. After that period the total volume is determined anda sample extracted in a sample bag. The s&mple (bag) js frozenand stowed in a container for return to earth in the CommandModule (CM). The urine bag containing the residual urine is removed

from the collection module, placed in a trash bag for eventualdisposal in the L0X tank by way of the trash airlock.In contingency urine collection the crewman micturates directlyinto the urine bag by way of an elastomer cuff. The bag isstowed in the collection module for a 2h-hour period. Again urineis collected for a 2h-hour period, volume determined, sampled,and disposed of as above.In fecal/diarrhetic collection a fecal bag is removed from itsstowage container and installed in the collection module. The

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crewman defecates into the fecal bag using entrained air flow toassist moving the bolus from the crewman into the bag. The usedbag is sealed, removed from the collection module and placed inthe Specimen Mass Mes_,urement Device (SMMD) where the the mass isdetermined. The sealed bag is then placed in the waste processorfor a given time (the time is a function of the mass) duringwhich the solid wastes are processed (dryed) by the combinedeffects of vacuum and heat. The processed material is thenstowed for return to earth via the command module,In vomitus collection and in contingency fecal collection thecrewman obtains a contingency fecal bag from its stowage containerand defecates/vomits directly into the bag. The bag is thensealed, mass determined, processed, stowed and returned to earth8.Sa_ove.In wet and dry material and refuse collection the crewman obtainstrash bags from stowage containers and mounts them in thefollowing locations : Waste management compartment Wardroom Sleep compartment Experiment compartment Forward compartment

Periodically as required filled bags are sealed and disposed ofinto the waste tank by wa_ of the trash alrlock.Design Concept-Trash Airlock - The ]281491 trash disposalairlock assemblM is basically a pass-through chamber built into

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the waste tank common bulkhead and extending through the floorinto the habitation area. Each side of the chamber is equipped

with a hatch, forming an airiock (Figures 2.2.11.1-3 through -6).The hatch on the habitation area side is subject to the habitationarea pressures and temperatures. In orbit, the waste tank is_rentedto space vacuum, and the hatch on that side of the airlock

is exposed to the waste tank temperature. The airlock is equippedwith a pressurization valve that allows its pressure to be equal-ized with that of either the habitation area or the waste tank,as required. The valve body contains the habiuation area ventin the form of a threaded female port which is also used as apressurization test port. In orbit, the trash disposal airlockis normally vented to the waste tank. The airlock body is spherical,approximately 24-inches (0.61 meters) in diameter, and has a pres-sure gage for crew observation. It is equipped with a mechanicalejector to accomplish the transfer of the waste material to thewaste tank. The functional steps of the operation cycle of trash

disposal from the habitation area are as follows: Valve/outer door handle - press 5 psi (34.5 kN/m2) (verify) Lid - unlock and open Insert trash bag Lid - close and lock Valve/outer door handle - close/vent [verify 0.5 psi (34.5 kN/m2)] Valve/outer door handle - open Ejector handle - eject return to close Valve/outer door handle - close/vent Ejector handle - retract

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A flow diagram of the six functions i_ pr,_sented in

Figure 2.2.11.1-7. Functional descriptions are presented in

Figure 2.2.11.1-8 through 2.2.11.1-11.i/ Waste Ms/lagement Supplies - W_ste management supplies for

collection of waste material conzist of fecal b=gs, con-

tingency fecal bags, urine collection provisions and con-

tingency urine cuffs to collect and to retain a crewman's

i body wastes. Collection bags are provided to support wastemanagement activities for normal operational usag,e, for con-

tingency tulle," "or,modes, and to facilitate hygienicwaste collection, waste processing and on-orbit storagt and/

: or disposal. Vacuum cleaner bags are _iso supplied to collect

and to retain cabin debris, and trash ba_,s are supplied tcthe collect refuse in habitable compartments.

Collection bags are com;tructed of an impermeable outermaterial with an openin, _ of sufficient _[ze to allow waste

material and air to enter (Figure 2.2.Ji.i-12). A vaporport on each collection bag (exce_,t t}'_eurine ba_-_)_llows

: air and vapors to pass throu_,_h :_nd exit the b:1_ The va_,oroort contains a millipore filter witil :_u_droph


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disposal. A data entry tag is provided as an integral partof t

msfc skylab orbital workshop, volume 3

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