NRO APPROVED FOR 

RELEASE 1 JULY 2015 

DOCUMENT CONTROL LOG . 

Control Number WHS-184 

Copy Number 

. 

Name of Courier 

Source • 

S. M. Tennant 

Addres see 

i 

i 

Description, Date, Subject, cy number, number of pages, any other identifying 

control number 

1 

Briefing booklet: xerox copies of MOL Engineering Baseline 

Description, dated 30 Jan 67 (presented to Mr. Gehrig & others 12/1/66) 

:Iktta.chrnents 

R.-n-narks 

File: SMT Safe 

Disposition' 

- Receipt Signature Date Inventory Date 

iiiit -l• o 7 Soeps4,......1" 

7 -x0.--ki 

. 17efi / 1 >7-7‘ 60/ 

, 

I 

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LEFT VIEWGRAPH 

4-4---Coatrp&etePe—Re•spensibilities 

RIGHT VIEWGRAPH 

BRIEFING OUTLINE 

• 

71. Title 

V 2. Schedule 

Inboard Profile - Manned Version 

Inboard Profile 

Mission Module 

6. Mirror Technology 

7. Tracking Mirror Gimbal Arrangement 

• 8. Direct View & Tracking System 

• 9. Acquisition Scope 

10. Readout System 

Payload Operations 

•12. Lab Vehicle Arrangement 

6.'13. Attitude Control & TS 

Environmental Control & Life Sup ort 

Structural Arrangement 

46. Electrical Power System 

v47. Communications & Data Handling 

$128. Gemini B 

3119. Titan IIIM 

1,20. Current Weight Status 

v""21. Aerospace Ground Equipment 

22. Aerospace Ground Equipment 

vt3. Laboratory Vehicle Flow 

724. Factory Test Program 

W.25. MOL Mission Simulator • 

26. LCC Master Control Room Equipments 

- 27. Schedule Chart 

/3. 

/4. 

V 5. 

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NRO APPROVED FOR 

RELASE 1 JULY 2015 

WFS-090 as of 11 January 1967 

MOL Engineering Baseline Description 

la. Purpose of MOL/Dorian System 

V. 2. Inboard Profile 

./ 3. Inboard Profile (Automatic) 

4. T3 Picture 

4a. Current Launch Schedule 

2.4 4b. General Schedule 

5. System Capabilities 

6. Mission Module 

7. • Payload Characteristics 

i 1 8. Payload Operating Capability 

9. Payload Sequence 

10. Sino Soviet Bloc Map 

11. Mission Control & Recovery 

12. Orbit Altitude Control 

13. Altitude Versus Latitude 

14. Coverage Pattern at 40° Latitude 

15. First Day 

16. Day N. 

17. Ground Contol 

18. MOL MCC 

19. Ascent Control 

20. Recovery 

21. East Fence Area 

22. West Fence Area 

Classification 

UNCL 

SSH 

SSH.C. 

SSH 

should be secret 

Unc. 

SSH 

SSH 

SSH 

SSH 

SSH 

SSH 

SSH 

Confidential 

SSH 

SSH 

SSH 

SSH 

SSH 

SSH 

SSH 

Uncl. 

Uncl. 

Uncl. 

Uncl. 

269-/ arkU7?)"-1) Le, 4-A ' 

25. Gemini B 

26. Attitude Control & Translation System war kr le.wift9 

27. Environmental Control & Life Support wet 4r 0/479 

27a. Structural Arrangement 

28 Communications/Data Handling ewEllE4st.77.2/sAre viht 

29. Electrical Power System toff iS Y. MT/ 

a-c930. MOL Weight & Performance Summary 

31. Development Milestones 

2.3 32. Lab Vehicle Hardware Flow 

11 33. Aerospace Ground Equipment 

34. Requirements for Simulation 

t 

I 

t 

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t7 

rb 

((EE 63--340,•44 Confidential 

Confidential 

Confidential 

Uncl. 

Secret 

Confidential 

Uncl (?) 

Uncl. 

SSH 

SSH 

Uncl. 

tIA14-11.• 
MOL ENGINEERING BASELINE DESCRIPTION 

NRO APPROVED FOR 

RELEASE 1 JULY 2015 MV11 (

arammna WHS-184 

30 Jan. 1967 

Copy I of f 

Total-Pages: 2 y 
CITR 

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A 

P DR 

GE 

DAC 

EK 

DESIGN • 

• 

1969 1967 

GE 

DAC 

EK 

1968 

ACCEPTANCE 

NRO APPROVED FOR 

RELEASE LY 2015 -SeettLiur - SPECIAL HANDLING 

,\Ah-s 

fl 2- 

GENERAL SCHEDULE 

DEVELOPMENT 

TESTING 

GE 

DAC 

EK 

LAUNCH 

F V #3 

QUALIFICATION 

TESTING 

GE 

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"Sreiteift SPECIA., HANDLING NRO APPROVED FOR 

RELEASE 1 JULY 2015 

SECRI3T SPECIAL HANDLING 
NRO APPROVED FOR 

'RELEASE 1 JULY 2015 

S CC RFT /SPECIAL HANDLING 

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• 8-15 Zi95 

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MIRROR TECHNOLOGY 

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P1 41 

• PRIMARY AND TRACKING MIRRORS 

• "EGG-CRATE" CONSTRUCTION 

• MATERIAL - FUSED SILICA 

• WEIGHT - 1020 LBS. EACH 

• THICKNESS - 

FACE PLATE 0.9 INS. 

BACK PLATE 0.5 INS. 

CORE 0.22 INS, 

• OPTICAL TOLERANCE -

-WAVE LENGTH 

EGG CRATES 

10.5 INS. 

'S - SPECIAL HANDLING ST-1059 

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RELEASER JULY 2015 
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ri1 TRACKING MIRROR GIMBAL SYSTEM 

I • 'Crew 

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ACTS 

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Signals r-- 

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Command 

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Encoders 

ACTS - ATTITUDE CONTROL/TRANSLATION SYSTEM 

ATS - ACQUISITION & TRACKING SCOPE 

BLOCK DIAGRAM 

SPECIAL HANDLING 

STIOS. • 
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Image Zoom Moving 

Elements 

First Ross 

Corrector 

Final Image 

Eyepiece 

Mirro 

Relay To Second Eyepiece 

Second Elemen 

Dove Mirror 

CHARACTERISTICS 

FIELD OF VIEW - 400 

ZOOM RANGE - 

GROUND RESOLUTION 

10' 

Platen 

Second Ross 

Corrector 

Pellicle • 

Second Ross 

Corrector 

(Visual Optics) 

SECRE T SPECIAL HANDLING • ST -1057 

Relay 

First Element 

Main Image 

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RELEASE 1 JULY 2015 

—SECRET SPECIA: *IANDLING 

DIRECT VIEWING AND TRACKING SYSTEM 
SECOND LOW POWER 

GROUP MECHANISM 

OUTER TUBE STRUCTURE ASSY 

INTERMEDIATE TUBE 

STRUCTURE ASSY 

ZOOM DRIVE MOTOR 

FILTERS 

FIRST LOW POWER GROUP MECHANISM 

D\ APERTURE STOP MECIAN ISM 

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CHARACTERISTICS: 

APERTURE 8" - 10" 

ZOOM RANGE 60X - 120X 

FOV 15X - 4o 

-ErEveltel" SPECIAL HANDLING 

MAX. GROUND RESOLUTION 3' 

WEIGHT ^r 500 LB 

,PEAK POWER — 500W izox - 0. s° 

NRO APPROVED FOR 

RELEASE 1 JULY 2015 

cECRET • Sm1CIAL HANDLING 

ACQUISITION AND TRACKING SCOPE 

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WIDE BAND READOUT 

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• WEIGHT "6 Sod 4.15,5 

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SECRET SPECIAL HANDLING 

NRO APPR D FOR 

RELEAS. 1 JULY 2015 

Wipe, 6N.N39 AIJA%.0 0r 

ENC)001- 

ST -1051 

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I' 1' 
PAYLOAD OPERATING CAPABILITY 

ACQUISITION AND TRACKING TELESCOPE 

LINE OF SIGHT SLEWING - 6 DEG/SEC 

SETTLING TIME - 3 SEC 

AUTOMATIC OPERATION - HANDS OFF OR UNMANNED 

PRECISION NAVIGATION 

• PRECISION POINTING (STAR TRACKER) 

• ELECTRO-OPTICAL IMAGE MOTION. COMPENSATION 

REAL TIME VISUAL OBSERVATION - MAIN OPTICS 

AUXILIARY PLATEN - SECONDARY FILMS 

READOUT - ANALOG - 800 IN. 2PER DAY 

ALIGNMENT - ANGULAR °- 1 MIN, LINEAR - .001 IN. 

FOCUS - AUTOMATIC - . 001 IN, PLATEN POSITION ACCURACY 

DATA RECOVERY - DRV - 60 LBS CAPACITY 

GEMINI - 240 LBS CAPACITY 

• CECItET SPECIAL HANDLING 

NRO APPROVED FOR 

RELEASE LY 2015 

SPECIAL HANDLING 
NROAPPROVED FOR 

RELEASE Y 2015 

LABORATORY VEHICLE ARRANGEMENT 

PRESSURIZED COMPARTMENT 

Consoles & Displays 

Crew Equipment 

Camera 

Film 

Film Handling 

Processors 

DR V's 

Computers 

ATS 

EC/LS 

Telemetry, Tracking, 

Communications, Voice 

ACTS Electronics 

UNPRESSURIZED COMPARTMENT 

Thruster Sectors 

Fuel Cells 

Propellants 

Cryogenics 

Heat Exchangers 

ECLS Pumps 

Crew Transfer Tunnel 

-ForirGAZZ' SPECIAL HANDLING 

ST- !®A1 

GEC= SPECIAL HANDLING 
..................................... ................... 

Namm=1;211 mmem 

• WASTE MANAGEMENT 

f. 

ATMOSPHERE CONTROL THERMAL CONTROL 

r7.77; 

• Ot/AL GAS AT/M257WERE,Oz BACH-6/P 

• 5 FSIA "011/RTSLECVE" • 

• 641PERC/FITICAL 02 STORAGE 

• MOLECGIZAIP o'/EVE Foe 492 CaYTKOC 

• 5 MINUTE COMPARTMENT 

Relife6611RIZ4PON 

• aPene seer toe FOR etweeoemor 

• HEAT EXCNAN6LW6 6 COLOPLATES 

• INNC/r WALL HEAT/N6 

• 5/34CE IrAP/ATOIr 

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• PROCESS 6 OTORE WAVE MATTER 

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NIRO APPROVED FOR 

RELEASE 1 JULY 2015 

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3 

—€10.4f-i9C-PeT•Md•- 11E+-4r,--Y41429-1-011 

ENWRONUENTAL CONTROL AND LIFE SUPPORT 

BASEL/NE LABORATORY I/Ell/CLE 
444444444444 

4 4 

4444444 

CRYOGENIC STORAGE 

• THREE /,000 HR. FUEL CELL MODULES 

• Z.0 KW AVERA6E POWER 

• 4,5 KW PEAK POWER 

• 3$ H2 AND rwo 02 74/1/KS 

• 130 DAY CAPACITY 

AEROSPACE CORPORATION 

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01CIA11‘110 NM 17 VIALS 

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NRO APPROVED FOR 

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11E.FalliSLIZIA8istitl 

ELECTRICAL POWERWER SYSTEM 

BASEL /NE LAB 1/ElaCCE 
NRO APPROVED FOR 

RELOIASE 1 JULY 2015 

STRUCTURAL ARRANGEMENT 

• 

UMW 

W 4S-1 

151 tc 

CORRUGATED SKIN 

COMBINED RADIATOR TUBE 

AND STIFFENING FRAME 

(12 REQUIRED) 

BEADED 

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MYLAR 

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( 6 REQUIRED IN FWD LM 

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INTERNAL SHELL 

UNPRESSUR- PRESSURIZED 

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LABORATORY MODULE MISSION MODULE 

atROSPACI CORPORATION 
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NRO A OVED FOR 

REL SE 1 JULY 201 

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ALT—W,—Y21 ishir R 

AEROSPACE CORPORAI ItiN 

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TITAN HIM DESCRIPTION 

MAJOR FEATURES 

• PERFORMANCE 

32, 800 LBS @ 800-80/130 N. MI, 

• TOTAL THRUST AT LIFTOFF - 3 MILLION POUNDS 

7 - SEGMENT SOLIDS 

• CORE - 2 STAGES 

NO TRANS TAGE 

STAGE 1 ENGINES - 15:1 NOZZLE EXPANSION RATIO 

▪ REDUNDANT FLIGHT CONTROL SYSTEM 

▪ BOOSTER INERTIAL GUIDANCE SYSTEM DURING ASCENT 

(BIGS) 

• GEMINI INERTIAL GUIDANCE SYSTEM BACKUP 

(GIGS) 

NRO APPROVEEOR 

RELEASE .1 JULY 2015 

TITAN.III M 

...wawa..• 
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• 3 

MOL WEIGHT AND PERFORMANCE SUMMARY 

BASELINE WEIGHT CURRENT STATUS 

(LDS) (LDS) 

6,068 6, 110 

5.630 5, 669 

360 360 

81 01 • 

14 , 000 14,166 

•Ima••./■•••■ . •■••••■■••••■•■■ 

LABORATORY MODULE 12,048 12,214 

MISSION MODULE STRUCTURE '1,952 1,952 

MISSION PAYLOAD 8, 439 

••

8,4 41 

■••••■•••■• 

MISSION MODULE EQUIPMENT 6, 226 6,280 

LABORATORY MODULE EQUIPMENT 2, 213 2,153 

'0 AL aBLEAL ER( L."4 

L. V. CAPABILITY (80°, 80/180, 55°N. WTR, T-IIIM) 

••■•••••■■■•■•••••• 

NRO APPROX'ED FOR ' 

RELEASE l'JULY 2015 111111111111‘411. 

\P II 

32, 27.0 

+3.1'53 I 

GEMINI B 

GEMINI B SEGMENT 

GREW 

PRESSURE SUIT ASSEMBLY 

LABORATORY VEHICLE 
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1%. 

CEC IIDT SPECIAL HANDLING 

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COMPLETE CHECKOUT OF EACH SYSTEM SEGMENT 

INDIVIDUAL SEGMENT AGE 

DESIGNS EXISTING 

USE AS IS 

T -IIIM 

GEMINI B 

wgs-itti 

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LABORATORY MODULE 

MISSION PAYLOAD 

SEPARATE, COMPUTER CONTROLLED 

--- OPERATE TOGETHER 

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- IDENTICAL AGE AND TEST PROCEDURES, FACTORY & PAD 

- OPTICAL TESTING AT ROCHESTER ONLY 

ET- SPECIAL HANDLING 

A 
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FACTORY TEST PROGRAM 

CONTRACTOR TESTS 

TEST 

SPECIMEN 

MMFS # 1F 

2F 

3F 

4F 

GE 

THERMAL 

STRUCTURAL DYNAMIC 

DEV ELOPMENT 

BUILDUP ONLY 

QUALIFICATION 

EK 

THERMAL 

ACOUSTIC 

DEVELOPMENT 

QUALIFICATION 

DAC 

STRUCTURAL = DYNAMIC /STATIC 

QUALIFICATION (EMC ONLY) 

MMAS # 1A 

2A 

3A 

4A 

LM . # 1 

# 2 

* NON-PRIME 

ACOUSTIC STRUCTURAL = DYNAMIC /STATIC 

THERMAL 

DEVELOPMENT 

QUALIFICATION 

ACOUSTIC /DYNAMIC /STATIC 

QUALIFICATION 

r SPECIAL HANDLING 
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COL 4/1/05YON 011kfULATOR 

GEM/N/ 8 MODS11.6 Smtut.treb tAfearAn2A7 

41001fle 

3/MULATOre 

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RELEASE 1 

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LABORATORY VEHICLE HARDWARE FLOW 

MOM 

wt.is -1q1 

P

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DOUGLAS 

HUNTINGTON BEACH, 

CALIFORNIA 

GENERAL ELECTRIC 

PHILADELPHIA,. PENNSYLVANIA 

EASTMAN KODAK 

ROCHESTER, NEW YORK 

MISSION MODULE STRUCTURE CAMERA OPTICS ASSY. 

DRIVE SERVOS ----) + 

LABORATORY MODULE 

PAYLOAD CONSOLES 

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• + 

THERMAL VACUUM TEST 

DIRECT TO PAD 

CLICREIT SPECIAL HANDLING . 

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DIRECTOR 

CONSOLE 

(COMM) 

ATW 

LAUNCH 

CONTROL 

CONSOLE 

(COMM) 

Wt4S--irr; 

I° 61 2-q 

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,4. 

LCC MASTER CONTROL ROOM 

HARDWARE 

CCTV MONITOR 

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(COMM) 

OV LAUNCH LAUNCH LV & COMPLEX PAD SAFETY RANGE 

CONDUCTOR CONTROL SUPPORT OFFICER SAFETY 

CONSOLE CONSOLE CONSOLE CONSOLE OFFICER 

CONSOLE 

(DAC) (MMC) (MMC) (COMM) (MMC) 

-4 

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CCTV AEROSPACE ATW MISSION 

CONTROL MISSION 

CONSOLE COCRDINATOR COORDINATOR 

CONSOLE • CONSOLE 

(COMM) (COMM) (COMM) 

CCTV MONITOR 

(COMM)