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SliMMARY Cost and ycrformancc technology hrcakthroughc it1 rcccnt ycarc havr niadc po\cihlc thc ncar icrm dcvclopnicnl and clcployincnt of a low cmt TACSAl \uncillaiicc \y\tt*in. Thc prtciitial rtrr hoth ihc \pacecraft and wnuir IO hc lauiwhcil cm loucr coi\t I:iuiicli \y\tcni\ I\ ihc funtlainsntal for rctlucccl \y\tcni ci~t. Acltlitionally. thc spiicccraft and scn\or iiiN hc anirnahlc III IOU' co\i maw protlucticin. Virr all weather. d;ry/night survcillancc. an activc synthetic :ipcrturc radar I$:\RI it thc ideal in\trumcnt. ancl thc obilily 1st masinanufacwc thour;ld% of vcry low ccnt iran\niii/rcccivc tT/R) IIIIJUIC\ ha% kcn dcvclopccl at H~phc*. Sincc ihc si/r of a SAR incrcasc.; ac thc orhital aliitudc is incrcarccl. b final clmcnt of thc cconcmicrl hviq for a low ciht 'I'A
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ADVISORY GROUP FOR AEROSPACE RESEAR
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Acccorclinp tto 11s C”liirlcr. th
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0 Im oyi.rationr rcccntc\ *Tcm+tc d
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Theme 'fieme 0 - 0 Avionics Pencl a
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-- Printed in Clawificcl puhlicatio
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1'. 2 c From tplc four pafcn. thcrc
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Talcs. Thc lcchnology emphasis wnr
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These arc three spccific fecornmen&
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when WO Rave gone from one'modsl sa
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3-4 mggd and easily operated. This
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3-6 interim capability should one o
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OI~UI'IS MISSIONS I PAYLOAD TYPE -.
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1 Int raduction The iiotcntial cxpl
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indicated hat an IR vcrsion of the
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a 0 Annex A Radar system A. I Backg
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Annex C ESM system C.1 Background A
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e communications, point to point, p
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(i-4 TACSAT Operations Phase The TA
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6-6 w J > a 3 v, [E ' 0 LL U3 I- Q
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(1-2 rcliabiliry pcrfornianccs, bot
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0 8-4 specific tools for each main
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0 0
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affichent un coot au kilo de 2 a 3
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I 1 - CONSTELLATION LAIJNCHES COST
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ls FIGURE 3 6-11
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a a
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SYmME DE NAVIGATION PAR SATELLIT'ES
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du sntcllitc fixCe. Aucunc controin
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0 0 ' ml 3200. 2800. 2400. 2000. 16
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A cct instant. ct si IC PDOP cat in
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giostationnaire (RS mlslnn contrc 5
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0 This pqxr is dividcd in lhrcc pat
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0 Grouad-air-ground communication T
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0 a .. . . .I AIR COMMAND AND CQNTR
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ENNEAAV ORDER OF BATLE ASSESSMENT D
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0 0 (CO") -COMMUNlCATlONTACSATSARE
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0 0 . 14-2 xiv)physical attack and
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14-4 There has been a minimum of jo
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Architecture TABLE -1 Number of Sat
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14-8 Table - 3 : The EHF Ground Seg
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0. 16-2 combincd analog and digital
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flgurm 2. Frequency Synlhmrlur Aduc
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L n , JA. " Flguro 5. LlghtwolgM LD
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GEOSYNCHRONOUSALTITUDEORBlT VARIABL
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I SYNCHRONIZATION TECHNIQUES FOR ME
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-U I 1 b I l l . . . . , Figure 2:
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@ & a time acquisition. Due to thc
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6 SYSIXM SYNCHRONIZATION ALGORITHM
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TACSAT payload. Sptinl and time syn
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\ I ..I , .. . . U' c L. rL 50 i !
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It is IqmmtQlive of the ,wc.sa Cmst
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I' !'.
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v / I ,p ,
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f I
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3. IAUWCUU SVSTEM SELECTION CRUQTXO
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19-41 5.8.1.8 A/Im faniity of whicl
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CURRLHT PRowcTKm N DEVELOPMENT " P
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.clrc;lih w m iua thc orhilot planc
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19-10 OcazO midm ~ r nof mp htb~rm
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19-12 0 'I% whicles must PW: lnunch
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8.3 Uniad KingdodWussia Inrtn'm HOT
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1P.16 'II-tcx chen@ngcnvimnmcntal c
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SPACECRAIT AND I.AIJNCII SIISlT.MS
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c Firvn 4. Horimld vrhiclr andpaylo
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H 8p~nwmd by DARPA ud will dcliwr8
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'ThcTauNt prylodckcoicwl inlnlactt
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20-10 (hcntercoaunnndma have ben di
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RESUME Puisque ks futun lanceun per
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. 232 CdcJ du IIIOIWYHI?~ Mmoeuvm m
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En rcvnnchc, m ce qui concemc la pe
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Lea masses d'ergoh pour les trois o
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- Figure 13 - Les orbiteo intermedi
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SVMMARy - rution inonly I5 monh. Qu
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I f igun 5-1 QulrUfar spcun@ syslrm
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?- I
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* Snull ground conlrol VMS 1s.a.a F
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.. 1. INTRODUCTION Attitude- and Or
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m, = f*U*d Whcn liquid bipropellant
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sensors, gyros) intorporated in the
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th: burn-our (or dry) mm and subsys
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23-10 between the modulator output
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23-12 . pcnsatc for thc imbact of l
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23-14 e I w 11 n IS n n a 41 U 9s M
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23-16 / Fig. 4.3.1: ICDS principle
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23-18 Communication Weat her - Oper
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23-20 r - .-_ -- - -. --_.._ I U i
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23-22 I .a * .o.s 8.2 am3 c 0.012 a
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PRW mrms lottrfrsa : UDir Bnterfscc
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24.2 CJ6Qh ion pl'b;pPelaion tho ap
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48 iao 4.b 11 8.2 19.3 26.5 88.6 C
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I I ! I i ~ I I I I I I I ! I I I I
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[ Z ] C. Purrotta, M.Bieconi, A. Bi
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I 23-2 2. ):SADLISG TF.CIISOLOGY PR
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124.1 PhwdAwmy Mimv.~tnhbkL.u#eApn(
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Lulrhd durimilr NASA md Navy p*bd o
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2s-a The paylord concept is distinc
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Page 378: ~Y!!?w!L Tho fnasibllity of install
Page 382: c_- XZiiK matelT. mloy ka>r*can h.i
Page 386 and 387: , i'or a typical 708 operating duty
Page 388: Tho ]Lo~ton boU& Of the Dfb-UFfliTf
Page 392 and 393: I I 0 I I I I I , For tn ainglo pla
Page 394 and 395: NovorthdanfS high frograonq CIQBfi~
Page 396: 008e~Ensrr witfa ~ bde~ec~ion s of
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Page 401 and 402: I I I I I ! I I I I I I ~ I I I I I
Page 404: 274 from soia may. For this mission
Page 408 and 409: =mitrioa~ ~ ~ h i frown ~ ~ e allei
Page 410 and 411: e The SAW must possess a raa)is$wet
Page 412: I I I ! 27-9 Different data rate: c
Page 416 and 417: In resent ears, industry made gr0fp
Page 418: I I I I I I , I .: I I I 27- 12 7.0
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Page 428: . FIQURE 2. REPRESENTATIVE OPERATIO
Page 434: mr a n problem. The pal was to Jcwg
Page 438: w 4 I Discussion Question: May you
Page 442: - SURVEILLANCE - ENVIRONMENTAL FLEX
Page 446: 31-4 spciri dtilrdo * beMsa 450 rd
Page 450: *APERTURE *FOCALLENmn OAS U STARINO
Page 454: Tb lSB in &a "heat" of ha TacSet sp
Page 458: : 0' 31-10 plovadm mglc apecity int
Page 462: 31-12 _. ’ Discussion Question: W
Page 466: 33-2 commander. Parameters sP iwter
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Figure1 World Met roroloKy -h Visib
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, Comment: TACSATS, 1 only as "truc
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. 1.
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