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: 
AttachmentSize
PDF icon CIA-RDP80M01133A000200030007-7.pdf834.25 KB
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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 Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7 Next 3 Page(s) In Document Exempt Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7 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 Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7 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 Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7 Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7 Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7 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 Approved For Release 2005/04/22 : CIA-RDP80M01133A000200030007-7 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 N .00 T N -l th T \x- z I I N N 00 m 0 r --r ...~ O O O z z z c~ -v -v r r D D z z m rn 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