R&D SOLUTION
Document Type:
Collection:
Document Number (FOIA) /ESDN (CREST):
CIA-RDP80M01133A000200030007-7
Release Decision:
RIPPUB
Original Classification:
S
Document Page Count:
31
Document Creation Date:
December 16, 2016
Document Release Date:
November 23, 2004
Sequence Number:
7
Case Number:
Content Type:
OUTLINE
File:
Attachment | Size |
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Body:
Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7
ENVIRONMENT
? COLLECTION
? PROCESSING
? ANALYSIS
? REPORTING
R & D SOLUTION
NSA and NRO review(s) completed.
PROBLEM
DEFINITION
? INTRODUCTION
? CONSTRAINTS
? TRENDS IN SIGNAL
SVL.(ELECTRONIC SYSTEMS GROUP
?~c-rop WESTERN DIVISION
Approved For Release 2005/04/
CONSTRAINTS (U)
rDP80 M 01133A000200030007-7
? SYSTEM COST
? MANPOWER LIMITATIONS
? FOREIGN REAL ESTATE
? SUPPORT COMMUNICATIONS
? PLATFORM LOCATION I OPERATION
>w1ELECTRONIC
WSTERND VI ION SYSTEMS GROUP
T 'NEIL
SECRET SPOKE
Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7
SIGNAL ENVIRONMENT TRENDS (U)
INCREASING SYSTEM CAPACITY
? SOVIET BLOC/PRC
? OTHER COUNTRIES
INCREASING USE OF FREQUENCY SPECTRUM
? DENSITY
? EXPANSION
INCREASING VARIETY OF SIGNAL MODULATIONS
? PSK
25X1
? DATA TRANSMISSION
? ENCRYPTION
INCREASING USE OF AUTOMATIC SWITCHING
MULTIPLE MEANS/PATHS
SECRET SPOKE
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Next 3 Page(s) In Document Exempt
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Approved For6l 6L2LIftiffWRIVA000200030007-7
PROBLEM AREAS
SOLUTIONS
e REMOTEIUNATENDED
SYSTEMS
25X1
M `,AAUu..AA ELECTRONIC SYSTEMS GROUP
nA ~~~o WESTERN DIVISION
Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7
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Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7
SIGNAL PROCESSING (U)
PROBLEM AREAS
SOLUTIONS
? INFORMATION EXTRACTION
? VOLUMES OF CONVENTIONAL
SIGNALS
? DATA SYSTEMS
? ENCRYPTION SYSTEMS
? LOAD SMOOTHING
? SIGNAL PARAMETER ANALYSIS
? DATA CORRELATION AND D I S PLAY
? SELECTIVE TASK I NGIM I S S ION MANAGEMENT
/~~..
AA (ELECTRONIC SYSTEMS GROUP
~ Po WESTERN DIVISION
A r F 20 04 _ I 2j?v :. ~07-7
SOLUTIONS
INFORMATION CORRELATION
EXTERNALS WITH INTERNALS
MULTIPLE SOURCE INPUTS
SITUATION RECOGNITION
EVENTS
TRENDS
ANOMALIES
FILE RETR IEVAL AND MAINTENANCE
DECI S I ON THEORY
a (ELECTRONIC SYSTEMS GROUP
IED fi WESTERN DIVISION
Approved For Release 2005/
-RDP80 M 01133A000200030007-7
PRESENT AND NEAR TERM STATUS (U)
COLLECTION
? OCEAN BASED PLATFORMS
? REMOTE UNATTENDED RECEIVER
? REMOTE GROUND SITES
PL 86-36
PROCESSING
ANALYSIS AND
REPORTING
? SMMS
? CONTROL ANALYSIS AND REPORTING CENTER
? CENTRAL ANALYS IS CENTER
M ?`',ELECTRONIC SYSTEMS GROUP
s VWESTERN DIVISION
SECHEY HANDLE VIA CO HINT CHANNELS
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Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7
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EMPHASIS ON FUTURE R & D (U)
REMOTE/
UNATTENDED
SYSTEMS
MISSION
MANAGEMENT/
ANALYSIS AND
REPORTING
? LOW COST
? FLEXIBLE DEPLOYMENT
? REDUCED LEAD TIME
? COMPACT
? LOW POWER DRA IN
? LOW POWER DRAIN
MICROELECTRONICS
? HIGH DENSITY
MASS STORAGE
? MICROPROCESSORS
? DELIVERY
? DECISION THEORY
? OPERATIONAL IMPACT ? PATTERN RECOGNITION
? USER ORIENTED ? INFORMATION STORAGE
7 7 AND RETRIEVAL
ELECTRONIC
ESTERN DIVISION SYSTEMS GROUP
S9LV Nco o I W
Approved For Release 2005/04/22: CIA-RDP80MOl13
25X1
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CHARTER
0 REQUESTED BY DIRECTOR, DDR&E
0 REVIEW PAST AND PRESENT STUDIES
25X1
? SUGGEST INNOVATIVE DESIGNS
? PROPOSE NEW SYSTEMS AND OPERATING CONCEPTS
25X1
CON U )ENT AL
Approved For Release 20~~/0 2C 01133A000200030007-7
MEMBERS
j CHAIRMAN: MR. JAMES W. PLUMMER
MR. MINORU SAM ARAKI
MR. M.W. JACK BELL
a DR. ROBERT S . COOPER
MR. WILLIAM T. HAMILTON
MR. CHARLES H.. HUNT
MR. FREDERICK H. KAUFMAN
MR. EDWARD OFFENHARTZ
D R. HAROLD A. ROSEN
DR. MICHAEL I. YARYMOVYCH
LT COL FRANK A. PAPAROZZI
UNDER SECRETARY OF THE AIR FORCE
LOCKHEED MISSILE & SPACE COMPANY
ROCKWELL INTERNATIONAL CORPORATION
DDR&E
BOEING AEROSPACE COMPANY
GENERAL ELECTRIC COMPANY
TRW SYSTEMS
GRUMMAN AEROSPACE CORPORATION
HUGHES AIRCRAFT COMPANY
CHIEF SCIENTIST, U.S. AIR FORCE
EXECUTIVE SECRETARY, U. S. AIR FORCE
CON p!DENTIAI
Approved For Re esige 5/0&2 1
ClA.-Bql2E1.f)Mf) . 40Q3AW7-- -
ACTIONS TO DATE
O BRIEFED BY SAMSO, NAVY, SAFISP, AND NASA
?CURRENT & PLANNED SYSTEMS
?TRANSITION PLANS
CONDUCTED INITIAL ANALYSES
?SHUTTLE OPERATIONS
? ORBITER I PAYLOAD INTERFACE
?SHUTTLE UTILIZATION
oSERVICING OF HIGH VALUE PAYLOADS
? S PACELAB
? FUNCTI ONS OF MAN
?IUS
?EFFICIENT USE OF SHUTTLE VOLUME
OTITAN III -SHUTTLE TRANSITIONING
?LARGE DIAMETER SHROUD
?SOL!D UPPER STAGES
Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7
RN; r ...Nf IA
,e L
CONS= EN1TIAL
Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7
CC :1 =I ENTI I.
COMMITTEE POSITION 011 PAYLOAD/ORGITER INTERFACE
? ORBITER MON!T~" FOR MAN SAFETY ONLY
? ORBITER COMMANDS LIMITED TO SAFEING. PAYLOAD FOR ABORT.
? NO PAYLOAD CHECKOUT PRIOR TO RELEASE
? USE EXISTING SATELLITE CONTROL FACILITIES
?COMPLEX ANALYSIS REQUIRED
?LARGE DOD /CONTRACTOR DECISION TEAM ON GROUND
G ORBITER STANDBY FOR ASSISTANCE AND RETRIEVAL
e KEEP INTERFACE SIMPLE TO MINIMIZE COSTS
C0NFI Ef\ITIAtI~.
-- --- - -App
Approved For Releas 2Z r 80MO1133A000200030007-7
SERVICING OF CURRENT HIGH VALUE PAYLOADS IN LOW EARTH ORBIT
? ON-ORBIT SERVICING OF EXPENDABLES DOES NOT APPEAR ATTRACTIVE
*DEDICATED SERVICING LAUNCHES WOULD BE REQUIRED BY THE WEIGHT
OF EXPENDABLES -MOST HIGH VALUE PAYLOADS UTILIZE SHUTTLE CAPABILITY
? HIGH DEVELOPMENT COSTS FOR AUTOMATED ON-ORBIT REPAIR DEVICES.
OFFSET POTENTIAL SAVINGS
? SATELLITE REPLACEMENT & RETURN CAN BE ACCOMPLISHED BY THE SAME
LAUNCH
? LOW VALUE OF SATELLITE RETURN & REFURBISHMENT DRIVEN BY
? TECHNOLOG I CAL OBSOLESCENCE. OF LONG LIFE HARDWARE
? POTENTIAL DAMAGE AND CONTAMINATION TO OPTICAL HARDWARE
DURING RETURN
0
C0N F-ID T I A I
A}~pr-0aied ~p _ 1- 7:_----?---
Approved For Release 20 1~101133A000200030007-7
SPACELAD BASIC HA D~~ A E ELE E TS
(t4ixed Hode
'HIGH QUALITY
WINDOW
FORWARD UTILITY
BRIDGE
EVA HATCH
PALLET/ORBITER
ATTACH FITTINGS
MODULE ORBITER
ATTACH FITTINGS
EXPERIMENT SEGMENT
SEGMENT JOINT INSULATION
CORE SEGMENT
CONHHDENTIAL
Approved Tory - - ...._..T. - ...., w T
Approved For Release 20 / ,q:-:! . ~ r 1 01133A000200030007-7
CW- yo i'
POTE NTIAL DOD SPACELAB USAGES
? DOD BASIC RESEARCH LABORATORY
? DEVELOPMENT TEST BED FOR DOD MISSION EQUIPMENT:
? SURVEILLANCE
? WEAPONRY
? NAVIGATION
? COMMUNICATIONS
? SATELLITE INSPECTION
? METEOROLOGY
? SPACECRAFT SUBSYSTEMS
? SHORT TERM OBSERVATION PLATFORM
o7 TO 30 DAY MISSION
r
C'
CONFIDENTIAL
L
Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7
FUNCTIONS OF MAN
? SUBSYSTEM DEVELOPMENT TESTING
? CRISIS MANAGEMENT OBSERVATION
? CAPTURE OF NON-COOPERATIVE SPACECRAFT
? RECOVERY OF PARTS OF SPACECRAFT
? DEPLOYMENT, ERECTION, & ASSEMBLY OF LARGE STRUCTURES
SECRET
Approved For Release Ifff R jFDP80MO1133A000200030007-7
HIGH ENERGY ORBITS STUDY
? FIVE YEAR DOD MISSION MODEL
? FIFTEEN HIGH ENERGY MILITARY MISSIONS
? .: ;%LUATED COMBINED MISSIONS TO MAXIMIZE SHUTTLE UTILIZATION
? COMPARED SOLID ROCKET MOTORS AND LIQUID STAGES
? CONSIDERED SHUTTLE LOADING AND PAYLOAD SUPPORT CONSTRAINTS
F-If 'MITIAI
Ap.pro\
Approved For Release g-"144.60", F1Fi 80M01133A000200030007-7
LAUNCH OF CURRENT DOD SPACECRAFT WITH THEIR PRESENT UPPER STAGE
65,000 Ib SHUTTLE
ORBITER CAPABILITY
I'It 'It I11111 //I////// / / f / II II
DSCS-1I
II I
FLTSATC
NTS
OM
FLTSATCOM
CONFIDENTIAL
RW
TRAN S
STAGE
Approved For-Release.-2 113*boogoombooz
60
0
00 50
0
LIMIT DUE TO C.G. CONSTRAI
F DSCS-II
S/C(2)
MODS
S/C
MAO -
CEN-
TAUR
BASED ON "DOD STS PAYLOAD INTERFACE STUDY", MDAC,
Approved jyffayfnfflff2, VMt r3A000200030007-7
(Space & Weight available for additional payload)
323
(26.9 FT)
743
(17,000#MAX),
COMPOSITE C.G. (49,124#) -'STA 1002;
32,124# INCLUDES WT. OF TWO DSCS- I1, TRANSTAGE & i
i TRANSTAGE CRADLE
582
1139
*(32,124#) `
Approved Ecu Refease_2:QO5/.0.
11069 1 1187, 1302
Approved For Release 2 041 , ~C ~p14QLM01133A000200030007-7
HIGH ENERGY ? ORBITS OBSERVATIONS
*CURRENT DOD MISSION MODEL RESULTS IN SHUTTLE LOAD
FACTORS OF 50% IN WEIGHT AND 30% IN VOLUME
OMISSION COMBINATIONS ARE LIMITED BY
? S H UTTLE BAY LENGTH
? DEFINED SPACECRAFT CONFIGURATION (LENGTH TO DIAMETER)
? COMPACTNESS OF UPPER STAGES
?DEFINED CAPABILITY OF IUS (LENGTH AND P/L)
? NORMAL LANDING AFTER ABORT C.G. AND CONSTRAINTS
O HIGH ENERGY 63? INCLINED MISSIONS CAN BE COMBINED WITH
SYNCH EQ MISSIONS FOR DUE EAST ETR LAUNCH
CON'Nd IDENTIAL
""""CPfIYt!~f17`3Wf'~~'i~fl"~}3t4YINtl'?RUt~4?"?
0 MINIMUM. IUS RDT&E DOLLARS -SINGLE, LOW COST STAGE TO MEET
DOD NEEDS
*SINGLE IUS FOR COMBINED DOD/NASA MISSION MODEL-MINIMIZE
CHANGES TO COSTLY DOD PAYLOADS
? EXPENDABLE CAPABILITY ONLY-PAYLOAD AND STAGE COMPATIBLE WITH.
CURRENT LAUNCH VEHICLES
COMMITTEE 'WHY IUS'' STUDY GROUND RULES
0 M I NIMUM TOTAL SATELLITE AND IUS NON -RECURRING AND RECURRING
DOLLARS
? MAKE MOST EFFICIENT USE OF SHUTTLE
? MULTI -MISSION FLEXIBILITY FROM SINGLE SHUTTLE LAUNCH
o SIMPLE TRANSITION FROM CURRENT BOOSTER TO SHUTTLE
? EFFECTIVE APPROACH TO GET SATELLITE DESIGNERS TO START DESIGNING
FOR SHUTTLE TODAY WITH OPTION TO FLY SHUTTLE OR CURRENT BOOSTER
o EXPENDABLE CAPABILITY ONLY
? FLY ALL 24- HOUR, 12-HOUR AND SUPER-SYNCHRONOUS MISSIONS FROM
ETR
C FI E-NTI L
-- -. .... Approved--F-ar-?ele; . 2A95f8W2 ARE)P89MG443-3 48 --
'S b
Approved For Release 2005/04/22 CIA-RDP880M01133A000200030007-7
Ell
ALL SOLID PERIGEE/APOGEE KICK MOTOR OPTION---.
? ADVANTAGE OF INDIVIDUAL SOLID MOTORS OVER I US :
? FEWER SHUTTLE FLIGHTS (31 vs 22)
*FLEXIBILITY IN MULTIMISSION SATELLITE PLACEMENT
? USE OF EXISTING ROCKETS FOR MOST MISSIONS (4 90 PERCENT)
? POSSIBLE COST ADVANTAGE
? AREAS OF CONCERN:
o KICK ROCKET DEVELOPMENT COSTS
? KICK ROCKET vs IUS INTEGRATION COSTS
? SHUTTLE SUPPORT STRUCTURE AND INTEGRATION COSTS
? DEFINITION OF NON-DOD MISSION MODEL
? KICK ROCKET INJECTION ACCURACY
? SHUTTLE UTILIZATION
C d`J H DENTiAL
__ Approved.,F_gr Release 20051O4/22.; CIA-131280M01 _~.~
Approved For Release 2 0 i OM01133A000200030007-7
_ ~~~
TITAN Ill-SHUTTLE TRAHSITIONING
? PROBLEMS
? SHUTTLE SCHEDULE UNCERTAINTY
? RELUCTANCE OF PAYLOAD PROGRAM OFFICES TO COMMIT TO SHUTTLE
? VOLUME AND WEIGHT CONSTRAINTS
? UNDETERMINED PERFORMANCE, SIZE, COST, AND SCHEDULE OF IUS
? POSSIBLE SOLUTION
? LARGE SHROUD ON TITAN III FAMILY
? SOLID AKM 1 PKM UPPER STAGE
C0I =IDENTIAL
_Approved For Release. 200 -
Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030O07-7
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Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7
Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7
C O D T A L
FLN
SHUTTLE PAYLOAD
CON $ . i_ I I I I J.-T
Approved For Releas0 2005/04/22 : C - 0"0030007-7
Approved For Release 2005 7 2I l T4\41133A000200030007-7
ETR TITAN III CAPABILITY
? CONFIGURATION
14 FT. D IA. SHROUD
? SOLID AKM I PKM SPIN STABILIZED,
e PAYLOAD CAPABILITY
T-I IID (SOLIDS T-IIIC
? LOW EARTH ORBIT *281500 LBS. ?27, 400 LBS.
? SYNCHRONOUS EQUATORIAL ? 4,500 LBS. ? 2, 700 LBS.
?COST
? DEVELOPMENT & QUALIFICATION $ 15.5M
-T-IIID & FACILITY $ 6.5
- AKM I PKM $ 9.0
? RECURRING AKM I PKM
$ 1.0M
CONFIDENTIAL
7-7
Approved For Release 2005/04/22: 000200030007-7
CODE
AIR FORCE ACTIONS
? PREPARATION FOR OCTOBER 1975 DSARC ON SHUTTLE
INCLUDES CONSIDERATION OF:
? TITAN IIID AT EASTERN TEST RANGE
? LARGE SHROUD ON TITAN III
? SOLID ROCKET TRANSFER SYSTEMS
COFHPE!!TIA
-- - - Approves For o ^^..., 2h
Approved For Release 2006/b44i-: CIA-f$bP 0M 01133A000200030007-7
CONTINUING EFFORTS
SHUTTLE APPLICATION TO
* GPS
? DSCS III
? MILITARY USES OF SHUTTLE
? NEW MISSIONS
? IMPROVED MISSION CAPABILITY
0 REDUCED COST
O C FI