NRO APPROVED FOR 

RELEASE 1 JULY 2015 

10 Sept 69 

Col Ford - 

As per our telecon, enclosed herein is the 

briefing (A) gave to NASA which you attended 

last week. 

I suggest we come up with a study number(s) 

for studies of possible use of DORIAN 

technology/hardware, etc. by NASA rather 

than proliferate DORIAN clearance ( documentation. 

I would//he happy to work on such a plan. 

HARVEY COIN 

SECRET DUNN otits 

111111,kk BYEMAN 
l; I ( 11 uuwan 

NRO APP FOR 

IRLEAS 1 JULY 2015 

LE VIA BsisinfAN im 

APPLICATIONS OF THE MOL 

ACQUISITION AND TRACKING SCOPE (ATS) 

TO NASA SPACE MISSIONS 
NRO APPRO Page 2 

RELEAS JULY 2015 

a:, 

BRIEFING PURPOSE 

0 DESCRIBE POTENTIAL UTILIZATION OF MOL ACQUISITION AND 

TRACKING SCOPE SYSTEM IN APOLLO LUNAR EXPLORATION 

AND APOLLO APPLICATIONS PROGRAMS 

BYEMAN tom sni 

DORiAlv • 
3tUK Page 3 

NRO APPR I DORAN 

RELEA 1 JULY 2015 

BRIEFING CONTENT 

O MOL ATS DESCRIPTION AND STATUS 

O POTENTIAL ATS APPLICATIONS TO NASA MISSIONS 

I VIEWING DEVICE 

OPTICAL SENSOR 

* PROPOSED STUDY BY THE AEROSPACE CORPORATION 

• 

lflA yEgAn 

CORM MIN 

b0111111 
NRO APPR 

RELEA 1 JULY 2015 

MOL ATS DESCRIPTION AND STATUS 

0 PHYSICAL AND OPTICAL CHARACTERISTICS 

MOL ATS INSTALLATION 

MOL ATS OPERATIONS 

CURRENT ATS STATUS-- 

• 

aNtoVEMAN 

-5E-eREf DORIAN 

J 

J LOU ' D-SSH 

Page 4 
FOLDING 

MIRROR e• 

AT3.- \A/5" HT (MOO 

ft:>rri 

CONTRoLs 

187 L. 

105 Lb. 

NRO APPROVED FOR 

RELEASE 1 JULY 2015 

._ DORIAN 

/ITS. PI-11115icAL CIAARACTI.-12.1TICS, 

D-SSH 

Page 5 

Tc::)TAL 2.92 1.13 

Luau VIA -NAN 

RcruiDORIMi 

,:4:AaAtO 
NRO APPR atjaj MAN Page 5bu 

MOL ATS WEIGHTS 

OPTICS 

✓ TRAC KING MIRROR ASSEMBLY 

✓ TELESCOPE 

/ FIXED FOLD MIRROR ASSEMBLY 

SHROUD • 

65 LBS 

78 

20 

15 

I WINDOW AND BEZEL 9 

187 LBS 

CONTROLS 

I GYRO AND GYRO ELECTRONICS 

I CONTROL STICKS 

I SUPPORT STRUCTURE • 

/ HARNESS 

/ DRIVE ELECTRONICS 

8 LBS 

4 

8 

25 

60 • 

105 

292 LBS 

RELEA 1 JULY 2015 
• Page 6 

NRO APRROVEDFOR. 

';RECE:55.7:41VSY`201 - - 

• .., . • •- 

DORIAN 

-OPTICAL SCHEMATIC 
U-SSH 

Page 7 

ASE 1 JULY 2015 

j 

NRO VECITOP tUKt I 1 DORM 

ATS OPTICAL CHARACTERISTICS 

APERTURE: 10 INCH UNOBSCURED DIAMETER 

• FOCAL LENGTH: 

MAGNIFICATION: 

i LOW POWER: 16 X TO 32.X, ZOOMCONTROL . 

HIGH POWER: 63.5 X TO 127 X,ZOOM CONTROL 

APPARENT FIELD OF VIEW: 60° 

■■• 

• REAL FIELD OF VIEW 

✓ LOW POWER: 2° (AT 32X) TO 4° (AT 16X) 

HIGH POWER: 0. 5° (AT 127X) TO 1° (AT 63. 5X) 

• RESOLUTION: 3 FT/LINE-PAIR FROM 80 N. MI. 
NRO 

R ASE 1 JULY 2015 

I DORIAN 

UWE VIA BYE11111 

CONTROL SYSTEM 

DORIAN -4 

Page7bu; 

ATS SYSTEM CHARACTERISTICS 

• POINTING ACCURACY: 0. 1 (. 95? 

LOS VIBRATION: 0. 5 SEC (PEAK TO PEAK) ABOVE 6 HZ (. 95 

IMAGE MOTION RATES: 48pRAD/SEC BELOW 6 HZ (. 95 p ) 

LOS SLEW CAPABILITY: 7 30°/SEC 

• 
- --11RerAPPROVED,Ff3K ;, 

- RELEASE 1 JULY 2015, 

• 

••• " 

MN VIA Bum ;- 

_ 
NRO APPROVED FOR 

RELEASE 1 J 

DUMAN 

MOL ATS INSTALLATION IN LAB MODULE 

. 

• . 

MIRRORS._ 

EARTH <=1 

SECRET iltimml 
11** SS I-I 3LCUL Page 8a 

NRO APPROVED FOR I ' dORIAN 

EASE 1-JULY 2015 

VISUAL DLSPLAY PROJECTOR CHARACTERISTICS 

MISSION FUNCTION: 

SCREEN: 

SCREEN BRIGHTNESS: 

PROVIDE VISUAL CUES TO ASSIST CREW IN 

IDENTIFICATION OF TARGET AND/OR TARGET 

ACTIVITY 

BACK-LIGHTED, 6 1/2 INCHES IN DIAMETER 

-0 TO 25 FOOT-LAMBERTS, ADJUSTABLE 

SELECTION CAPABILITY: COMPUTER OR CREW COMMANDS CAUSE ANY 

ONE OF UP TO 32, 752 FRAMES TO BE PRFSENTED 

CUE CASETTES: EACH CASSETTE CONTAINS 4094 - 16 MK FRAMES, 

ON REELS 

RETRIEVAL TIME: 0. 45 ÷ N/100 SECONDS, IF CASSETTE INTELLIGANCE 

NOT REQUIRED 

N = NUMBER OF FRAMES FROM PREVIOUS TO NEXT 

CUE 

WEIGHT: PROJECTION - 23 LBS, CASSETTE 1. 2 LBSmut 
NR 

EASE 1 JULY 2015 

ATS/MAN'S ROLE (MOL MISSION) 

ORGAN 

INCREASE QUALITY OF TECHNICAL INTELLIGENCE BY REAL- TIME 

EVALUATION OF TARGETS 

G EACH CREWMAN WITH ATS VIEWS UP TO FOUR ALTERNATE TARGETS 

AND "VOTES" AS FOLLOWS. 

REJECT (PROBABLY CLOUD COVERED) 

INACTIVE (TARGET CLEAR BUT NO TI FEATURES OF 

INTEREST) 

ACTIVE (TI INTEREST) 

OVER-RIDE (INTERUPT PROGRAMMED MAIN OPTICS) 

Page 9 

D-551-1. 

• , 

s.b.r4.1.*41, 
tom —JJS1 

• ' 

NRO APPROVED FOR • ; t 4 • 

• i 

RELEASE 1 jUL2016 ! . . 

• -3 . ; - f 

uunuur Page 10, 

- 

CONCEPT OF MANNED EXAMINATION 

FOR, 

•

TECHNICAI., INTELLIGENCE INDICATORS/WEATHER 

: . 4 

ATS 

Ao • 

IF EITHER ALTERNATE HAS ACTIVE INDICATORS, TAKE IT 7. r • 

IF PRIMARY COVERED AND ALTERNATE CLEAR, SWITCH TO ALTERNATE__ 4 • • 

• 
NANDLE VIA BYEMAN 

Anozsysia_._ 

DECIDE 

SETTLE 

fit • -4.••• 

ta- do. 

'?iso 

• 

ts 

ACTIVE INDICATOR EXAMINATION AND SPECIAL PHOTOGRAPHY SEQUENCE 

NVO APPROVED FOR 

RELEASE 1 JULY 2015 

DORIAN Page 11 

i 

i 

- 
Page 12 

LE VIA 

4 YS DORIAN • 411 II 

ti 

ATS PROGRAM STATUS, JUNE 1969 

OPTICAL DESIGN COMPLETE 

0 OPTICAL TESTS ON BENCH UNIT COMPLETE 

J DESIGN PREDICTIONS VERIFIED 

FABRICATION OF OPTICAL ELEMENTS FOR TWO 

ENGINEERING UNITS: 95% COMPLETEMECHANICAL DESIGN:, 75% COMPLETE _- 

ENGINEERING MODEL COMPLETION 

SCHEDULED AUGUST 1969. 

NRO 9arRovLU Fox ttidel-- MAN 

REJ ASE 1 JULY 2015 
O APPROVED FOR 

RELEASE 1 JULY 2015 

POTENTIAL ATS APPLICATIONS TO NASA MISSIONS 
J. 

OCAAL Page 14 I IRMIPM 

NRO 

R ASE 1 JULY 2015 

POTENTIAL ATS RELATION TO APOLLO APPLICATIONS PROGRAM 

• .• • • . 

TASKS ASSIGNED TO ATS ABOARD AAP SIMILAR TO ATS FUNCTIONS 

ABOARD MOL: 

✓ VIEW EARTH (OR SPACE) FEATURES AND RECORD DATA 

✓ DIRECT OTHER SENSORS TO TARGETS ACQUIRED BY ATS 

ATS CAN BE USED AS A VIEWING DEVICE BY THE CREW, AND AS A 

PHOTO-OPTICAL AND/OR ELECTRO-OPTICAL SENSOR 

ATS OF PARTICULAR VALUE TO EARTH SURVEY TASKS (EG: 

AGRICULTURAL, GEOGRAPHICAL, GEOLOGICAL, OCEANOGRAPHIC) 

REQUIRING LESS THAN 50 FT. GROUND RESOLUTIONS 

ATS RECORDED DATA CAN BE RETURNED TO EARTH VIA WIDE- BAND 

TRANSMISSION LINKS OR DIRECT RECOVERY 

Offirin RANDLE VIA, BYEMAN 

mut ram. 

•■•••••■•••••010. 
DOR 11

L UV I 

Page 15 

NRO ARP nvFn Fni:z 

REL SE 1 JULY 2015 

TYPICAL EARTH SURVEY TASKS REQUIRING LESS THAN 

50 FT GROUND RESOLUTION 

COLOR 

DESIREABLE • 

...■••■■■■■•■•■•, 

CATEGORY TASK 

COLOR 

DESIREABLE 

AGRICULTURAL GEOGRAPHICAL 

X 

X 

Crop Identification 

Timber Inventory _ 

Land Use Surveys 

Rangeland Surveys 

Groundwater Survey 

Volcanic Eruption 

Assessment 

Mineral/Petroleum 

Survey 

Heavy Metal Survey 

Earthquake 

Assessment 

River Basin Mapping 

Water Pollution - 

Survey 

Sedimentation Survey 

Erosion Survey 

Flood Mapping 

Geological Mapping, 

1:250, 000 Scale 

Transportation Survey 

Industrial Survey 

1:24, 000 Sc ale 

Mapping 

1:62, 500 Scale 

Mapping 

1:250, 000 Scale. 

Mapping 

Settlement Planning 

Commercial Fish 

Location 

Sea State Survey, 

Coastal Mapping 

Coastal Engineering 

Survey 

Navigation Hazard 

' Survey 

Marine Pollutant 

Survey 

GEOLOGICAL 

X 

X OCEANOGRAPHIC 

X 

X 

X 

TASK 

- SECRET DORim CONTROL SYS1D1 
OPTICAL SCHEMATIC 

MOLE VIA ByEmAN EGRET DORIAN CON1110t SOU 

tt Kt I DEAN 

JIG HE 

OW OBJECTIVE L LOW 

LENS POWER 

GROUP 

NR APPROVED FOR 

RE ASE 1 JULY 2015 

FIXED 

MIRROR 

DEROTAT ION PRISMIMAGE pi,NNE 

FILM 

DRIVE 

----FIELD FLATTENER (2) 

IMAGE PLANE RETICLE 

TRACKING 

MIRROR 

FLIP 

MIRROR 

Page 16 

PEPRE*ENTATIVE- AT5/AA P CON F IgURATIONI 

ZOOM LENS 

FILTERS 

EYEPIECE 

IMAGE PLANE 
NRO AP RILVPD FCIR 

RE SE 1 JULY 2015 

Ell,KL I DORIAN Page 17 

ATS CAPABILITY FROM 240 N. MI. EARTH ORBIT 

F. O. V. 

I ZOOM 

f 

ZOOM 

1/2° 

MAGNIFICA TION VISUAL 

GROUND 

RESOLUTION 

(FT. ) 

PROJECTED 

F. O. V. 

DIAMETER 

(N. MI. ) 

PHOTOGRAPHIC 

GROUND 

RESOLUTION 

(FT. ) 

16 x 57 18 31. 0 

32 x 30 9 

63. 5 x 15 4. 5 7. 8 

127 x 9 2. 3 

V 

DORIAN. - ImPLE SECRET .107. 
NRUEPROVED FQR_ 

r

<LEASE 1 JULY 2015 

WIDE-BAND DATA TRANSMISSION FROM LOW- EARTH 

ORBIT USING DATA RELAY SATELLITE 

••••••••••■••••• •■•••■•■■••••■■■•■•■■•-■".... 

TRANSMISSION 

RATE DATA 

FRAME FRAME AREA 

RESOLUTION PER MINUTE 

(LP/MM) (IN2

) 

O O. 

50 

50 

100 

10 MHz 

25 MHz 

10 MHz 

25 MHz 

108 

275 

27 

100 67 

- 

H. 

5 

25 

1 . 2, 

6 

50 - 

50 

100 

100 

10 MB/SEC 

50 MB/SEC - 

10,MB/SEC 

50 MB/SEC 

r-Osolle",70. 

. — - 

DIGITAL BASED ON 5 BIT PCM, NO COMPRESSION , 

13 

1J-456H 

a Page 1 7bu 

.1147111A 
Page 18 

NRO A aCital DORIAN 

RE SE 1 JULY 2015 

POTENTIAL ATS RELATION TO. LUNAR EXPLORATION PROGRAM • 

ATS CAN BE USED BY THE APOLLO CREW TO MAKE DETAILED VISUAL 

SURVEYS OF THE LUNAR SURFACE AND RECORD SELECTED OBJECTS, 

SITES, AND REGIONS 

LANDING SITE EVALUATIONS 

i HIGH RESOLUTION MAPPING 

✓ LOCATION/IDENTIFICATION OF SURFACE OBJECTS 

(VEHICLES, GEOLOGICAL DETAILS) 

"LOW LIGHT" ELECTRO- OPTICAL SENSORS WOULD ALLOW INVESTIGATIONS 

OF POLAR AND TERMINATOR• REGIONS AND CRATER. SHADOWS 

TS RECORDED DATA CAN BE RETURNED TO EARTH VIA WIDE-BAND 

TRANSMISSION LINKS OR DIRECT RECOVERY 

DORIAN • MA 14/1 WA INMAN 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 SECRE DORIN 

TYPICAL CSM ATS INSTALLATION 

COMBINED LUNAR LANDING/MAPPING MISSION 

D-SSH 

Page 19 
OBJECTIVE 

LENS E Of 7 n 

)------I LIU Low uLIU 

PoWER 

GROUP 

FIXED 

MIRROR 

FLIP 

MIRROR 

TRACKING 

MIRROR 

Jcuftc. 1 DORIAN N RR O E EA AP SP ROVED F(r EJ_y2 

 ip. EPRE,ENTATIvE C SM C ON Fl GU eATl 0 tD- SSH 

Page 20; 

OPTICAL 5cHEMATIC 

FIELD:?FI.ATTENER 

Z00 '-P/MM

IMAGE PLANE 

FILM DZIVE 

cFIELD FLATTENER _ 

IMAGE PLANE ,r- RETICLE 

VIDICON I TUBE) 

• 40 LP/mm 

DISPLAY CONTROL 

CONSOLE 

(cm) 
TYPICAL ATS LUNAR OBSERVATION CAPABILITY 
RELEASE 1 JULY 2015 

LUIZ I DORIAN Page 22 

LUNAR LANDING SITE INSPECTION SCENARIO 

iPOLLO CSM L*. s. • 

LANDING 

3ITE 

O 10 N. M. ORBIT 

411 LOCATE LANDING ZONE WITH LOW POWER ATS 

O DISPLAY IN CM AND MISSION CONTROL 

+I 2400' FOV 

O CENTER LANDING SITE SCENE ON DISPLAY 

O SWITCH TO HIGH POWER ATS 

Il 600' FOV 

O CONFIRM LANDING SITE 

I MISSION CONTROL 

APOLLO CREW 

• LM DESCENT ON SUBSEQUENT ORBIT 

ALTERNATIVE LANDING ZONE/SITE EXAMINE 

DORiAN 6,U VIAfiTEhIi1:1 

II 
VIDEO DATA RESOLUTION 

2. 3 FT @ 20 N. Mi. 

VIDEO TRANSMISSION 

ANTENNA 

------------- 

L. O.S. TRANSMISSION 

0 VISUAL DISPLAY 

VIDEO ELECTRONICS 

CAMERA & FILM 

OPTICAL SYSTEM 

APOLLO CS.M 

PHOTO DATA RES. 

OPTICAL FIELD 

OF VIEW . 

EARTH 

AREA RECORDEDe MOON 

- 4 D-SSH 

Page 23 

RELEASE 1 JULY 2015 

LUNAR SURFACE OPTICAL DATA ACQUISITION 

• 

0 REAL TIME VIDEO INFORMATION 

0 STORED FILM RECORD 
O RETRIVE FILM FOR RETURN TO EARTHIN COMMAND_MODULE 

SECRET D°RIAN Man SYS! 

SEC ttt r IJURN 

/-:E7E777777f075 

ID-SSH 

Page 

a 

TYPICAL LUNAR SURFACE OPTICAL DATA ACQUISITION SCENARIO 

O ACTIVATE SYSTEM FOR LUNAR OPERATIONS, I. E. EXPOSE OPTICAL HEAD, 

CHECKOUT MECHANISMS, VERIFY FILM AND ELECTRO- OPTICAL SYSTEMS 

OPERATION 

O IDENTIFY LUNAR GEOGRAPHICAL AREA OF INTEREST USING CUE DATA 

O POSITION OPTICAL SYSTEM TO PLACE AREA OF INTEREST IN OPTICAL 

FIELD OF VIEW 

O PERFORM IMAGE CENTERING OF TARGETS AS. REQUIRED... • - 

O INITIATE DATA ACQUISITION MODE(S) FOR ELECTRO- OPTICAL SCENE 

RECORDING OR FILM/CAMERA OPERATION 

O CONTROL QUANTITY OF DATA COLLECTED BASED ON VISUAL, 

 OBSERVATION 

OF CONDITIONS AFFECTING PHOTOGRAPHIC OPERATIONS 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 S R DORM 

Page 25 

$41• 

CONCLUSIONS 

APPARENT NEED FOR AN A. T. S. ON NASA MANNED SPACE 

PROGRAMS HAS BEEN IDENTIFIED 

SYSTEM DESIGN ESSENTIALLY COMPLETED ON D. 0. D. MOL. 

PROGRAM 

ADAPTABILITY OF A. T. S. TO NASA MISSIONS APPEARS 

FEASIBLE BUT DETAILED STUDY NEEDED TO PROVIDE 

IMPLEMENTATION PLANS 

INTIMATE PARTICIPATION IN ATS CONCEPT AND DEVELOPMENT 

MAKES AEROSPACE _CORPORATION LOGICAL CONTRACTOR TC) 

PERFORM STUDY FOR NASA ON EFFECTIVE ATS UTILIZATION 

NAKE BYEMAN 

mot-Aysom 
JLA) 

RELEASE 1 JULY 2015 

AEI 

PROPOSED STUDY BY THE AEROSPACE CORPORATION 

•EPHASE I - SYSTEM DEFINITION 

I I PHASE II - GSE/TD OF CONTRACTOR EFFORT 
Tc, 

MANNED SPACE SYSTEM BACKGROUND 

DORIAN CONTROL MEM 

RELEASE 1 JULY 2015 

ocutIt. 

• PP • I II I DORIAN Page 27 

THE AEROSPACE CORPORATION, SINCE ITS FOUNDING, HAS BEEN ACTIVE IN MANNED 

SPACE SYSTEM ANALYSES. 

• COMPARATIVE STUDIES OF GEMINI, APOLLO'AND DYNASOAR 

• DOD/NASA GEMINI EXPERIMENTS PROGRAM 

• ATLAS, GLV, TITAN III LAUNCH VEHICLES 

o CONCEPTUALIZATION, GENERAL SYSTEMS ENGINEERING AND TECHNICAL 

DIRECTION OF USAF MANNED SPACE PROGRAMS 

/ MANNED ORBITAL LABORATORY 

THE CORPORATION HAS BEEN ENGAGED IN THE DESIGN AND SIMULATION OF CREW 

VIEWING SYSTEMS SINCE 1964. 

• POINTING AND TRACKING SCOPE (MOL EXPERIMENTS) 

• ACQUISITION AND TRACKING SCOPE (MOL PROGRAM) 

F 

• r 
COST, SCHEDULES, AND_SPECIFICATIOW-77, 

AIAN Page 28 

RELEASE 1 JULY 2015 

• I, 

- - STUDY SCOPE 

O INVESTIGATE THE APPLICATION OF THE ATS TO NASA SPACE MISSIONS 

AND VEHICLES 

APOLLO APPLICATIONS PROGRAM 

/ LUNAR EXPLORATION PROGRAM 

• ' • 

O DEVELOP MULTIPLE USES OF THE ATS - 

CREW VIEWING DEVICE 

PHOTO AND ELECTRO-OPTICAL SENSOR (NORMAL AND "LOW- LIGHT" 

SCENES) 

/ NEAR REAL TIME DATA TRANSFER 

O DEFINE NASA ATS CONFIGURATION AND OPERATIONS 

ATS DESIGN 

VEHICLE INTEGRATION 

CREW TRAINING 

7 

11, 
I MISSION OBJECTIVES 

/ ORBIT SELECTION CRITERIA 

/ OPERATING MODES 

/ CREW TASK ANALYSIS 

/ TOP. TIME LINE DEFINITION 

/ SIMULATION/TRAINING REQUIREMENTS 

✓ IMPACT OF ATS ON CURRENT MISSION PLANS 

O FLIGHT VEHICLE INTEGRATION STUDIES 

ATS CONFIGURATIONS ANALYSIS 

/ INSTALLATIONS ANALYSIS AND LAYOUTS - 

/ VEHICLE SUBSYSTEM IMPACTS 

/ SYSTEM COMPATIBILITY ANALYSIS/SUMMARY 

O SPECIFICATION DEVELOPMENT 

I BASIC OPTICAL SYSTEM 

1 PERIPHERAL RECORDING EQUIPMENT 

,INSTRUMENTATION 

/ COMPUTER HARDWARE/SOFTWARE 

/ POTENTIAL MODIFICATIONS 

/ TEST REQUIREMENTS 

O TRAINING PROGRAM AND EQUIPMENT REQUIREMENTS DEFINITION 

O PROGRAM IMPLEMENTATION PLAN 

O DEVELOPMENT AND ACQUISITION COST ESTIMATES 

DORIAN Paid Viil 

4ePage 29 

NR 0 PPrIVFLI PnR 

EASE 1 JULY 2015 

ATS APPLICATIONS 

(1)I STUDY TASK AREAS 

O NASA PLANS AND HARDWARE (APOLLO AND AAP) REVIEW 

/ OPERATION PLANS, TIMELINES, PERFORMANCE TRADES 

/ VEHICLE SYSTEM DESIGN CHARACTERISTICS AND CONSTRAINTS 

O MISSION APPLICATION AND PERFORMANCE ANALYSIS 
NR ROVED FOR 

EASE 1 JULY 2015 

page SU 

A TS APPLICATIONS 

PHASE I STUDY PROGRAM PLAN 

1970 1969 

F i TASK AREAS S 0 

O NASA PLANS & HARDWARE 

(APOLLO & AAP) REVIEW 

O MISSION APPLICATIONS & 

PERFORMANCE ANALYSIS 

FLIGHT VEHICLE INTEGRATION 

STUDIES 

O SPECIFICATION DEVELOPMENT 

O TRAINING PROGRAM & EQUIPMENT 

REQUIRED DEFINITION 

O PROGRAM IMPLEMENTATION PLANS 

O DEVELOPMENT & ACQUISITION 

COST ESTIMATES 

O DOCUMENTATION 

O REPORTS-- 

1 

P. If . FINAL. P.R. 

TERM 

SECRET DOR 

F•1 r.I 

ETC 
NRO APP 

RELE 1 JULY 2015 

- z m Page 31 

ATS APPLICATIONS 

PHASE I STUDY MANPOWER ESTIMATE 

1969 1970 

TASK AREAS I s 1 0 1 N D F 

O NASA PLANS & HARDWARE 

(APOLLO & AAP) REVIEW 

O MISSION APPLICATIONS & 

PERFORMANCE ANALYSIS • 

O FLIGHT VEHICLE INTEGRATION 2 

STUDIES 

4 

O SPECIFICATION DEVELOPMENT 

O TRAINING PROGRAM & EQUIPMENT 

REQUIRED DEFINITION 

O PROGRAM IMPLEMENTATION PLANS a 

O DEVELOPMENT & ACQUISITION 

COST ESTIMATES 

0 DOCUMENTATION 

8 8 6 40)- TOTAL MAN MONTHS 

r• 

SECRET Dow