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Figs. 2.1- la-2.1- IC: Parmeters for sun-synchronous orbits figs. 2.2-1a/b: Principle Sic-solar rurav configural ion I i -w w fig. 2.1-2: 23-13 IO0 1001 -(Y 100000 IOOOOOO Number of LEO satellites required for global coverage (10" elevation from ground) Fig. 2.1-3: Drag' factor versus altitude 100000 200000 100000 400000 500000 600000 Fig. 3.2-3: Trade-off mono-hipropellant thrgster cfficicncy versus total impulse
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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
Page 277: - Figure 13 - Les orbiteo intermedi
Page 281: SVMMARy - rution inonly I5 monh. Qu
Page 285: I f igun 5-1 QulrUfar spcun@ syslrm
Page 293: ?- I
Page 301: * Snull ground conlrol VMS 1s.a.a F
Page 305: .. 1. INTRODUCTION Attitude- and Or
Page 309: m, = f*U*d Whcn liquid bipropellant
Page 313 and 314: sensors, gyros) intorporated in the
Page 316: th: burn-our (or dry) mm and subsys
Page 322 and 323: 23-10 between the modulator output
Page 325: 23-12 . pcnsatc for thc imbact of l
Page 331 and 332: Fig. 4.1-1 a/h: SIC orientation U2
Page 333: 4 2 0 -2 -4 t . . . I "W Fig. 4.4-1
Page 337: Control Accuracy 1 Control oncep pi
Page 341: 0.75 - 0.2 2 - 0.6 6 - 1.85 IO - 3
Page 345: abic 4.2-2: Corrcspadaucc bcwccn to
Page 349: lpnpQR rOYi0WS the QdVOUItQ~OQ and
Page 352 and 353: 3.2 P A tuimira ~ ok c~,~~a~aellona
Page 354 and 355: Thoro are sovoral additlonal positi
Page 356 and 357: - it is possible to use 8 low level
Page 358 and 359: I . Ihfcmc Advanced RcJcuch hojccts
Page 360: - physical and mvirnnmmtal rrquirem
Page 364: IMPACT rill work cbuly wilh thr MIL
Page 368: ! --- ----FE- UICLIEASWO SAIEI Ill
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I 0 I I I @. I 1 @uc?otion: You men
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aLRaqy1 rsmnto ,.verviaw An incrooa
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264 giving tho nunbor of oaeollitnn
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0 I
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280 65.0 63:6 40.1 360 84.6 81.8 56
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I I I
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I I I
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The small size aaad low mts of the
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The dediated nature of the sumeiUUa
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274 The outhe cdmcept of a SAR moun
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In order to erform a useful recoanw
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I I
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-.- I I I I I !
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27-10 Currcunaly available ground a
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I ! I I I I I
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Figure 1 Figure 2 \ '. 0 # --e- I i
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SliMMARY Cost and ycrformancc techn
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. FIQURE 2. REPRESENTATIVE OPERATIO
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mr a n problem. The pal was to Jcwg
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w 4 I Discussion Question: May you
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- SURVEILLANCE - ENVIRONMENTAL FLEX
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31-4 spciri dtilrdo * beMsa 450 rd
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*APERTURE *FOCALLENmn OAS U STARINO
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Tb lSB in &a "heat" of ha TacSet sp
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: 0' 31-10 plovadm mglc apecity int
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31-12 _. ’ Discussion Question: W
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33-2 commander. Parameters sP iwter
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, I I I : I I 33-4 . I. psitiom am
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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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