- Page 1:
ADVISORY GROUP FOR AEROSPACE RESEAR
- Page 5:
Acccorclinp tto 11s C”liirlcr. th
- Page 9:
0 Im oyi.rationr rcccntc\ *Tcm+tc d
- Page 13:
Theme 'fieme 0 - 0 Avionics Pencl a
- Page 17:
-- Printed in Clawificcl puhlicatio
- Page 21:
1'. 2 c From tplc four pafcn. thcrc
- Page 25:
Talcs. Thc lcchnology emphasis wnr
- Page 29:
These arc three spccific fecornmen&
- Page 33:
when WO Rave gone from one'modsl sa
- Page 37:
3-4 mggd and easily operated. This
- Page 41:
3-6 interim capability should one o
- Page 45:
OI~UI'IS MISSIONS I PAYLOAD TYPE -.
- Page 49:
1 Int raduction The iiotcntial cxpl
- Page 53:
indicated hat an IR vcrsion of the
- Page 57:
a 0 Annex A Radar system A. I Backg
- Page 61:
Annex C ESM system C.1 Background A
- Page 65:
e communications, point to point, p
- Page 69:
(i-4 TACSAT Operations Phase The TA
- Page 73:
6-6 w J > a 3 v, [E ' 0 LL U3 I- Q
- Page 77:
(1-2 rcliabiliry pcrfornianccs, bot
- Page 81:
0 8-4 specific tools for each main
- Page 84 and 85:
0 0
- Page 87:
affichent un coot au kilo de 2 a 3
- Page 91:
I 1 - CONSTELLATION LAIJNCHES COST
- Page 95:
ls FIGURE 3 6-11
- Page 98 and 99:
a a
- Page 100:
SYmME DE NAVIGATION PAR SATELLIT'ES
- Page 104:
du sntcllitc fixCe. Aucunc controin
- Page 108:
0 0 ' ml 3200. 2800. 2400. 2000. 16
- Page 112:
A cct instant. ct si IC PDOP cat in
- Page 116:
giostationnaire (RS mlslnn contrc 5
- Page 120:
0 This pqxr is dividcd in lhrcc pat
- Page 124:
0 Grouad-air-ground communication T
- Page 128:
0 a .. . . .I AIR COMMAND AND CQNTR
- Page 132:
ENNEAAV ORDER OF BATLE ASSESSMENT D
- Page 136:
0 0 (CO") -COMMUNlCATlONTACSATSARE
- Page 140:
0 0 . 14-2 xiv)physical attack and
- Page 144:
14-4 There has been a minimum of jo
- Page 148:
Architecture TABLE -1 Number of Sat
- Page 152:
14-8 Table - 3 : The EHF Ground Seg
- Page 156:
0. 16-2 combincd analog and digital
- Page 160:
flgurm 2. Frequency Synlhmrlur Aduc
- Page 164 and 165:
L n , JA. " Flguro 5. LlghtwolgM LD
- Page 167:
GEOSYNCHRONOUSALTITUDEORBlT VARIABL
- Page 170:
I SYNCHRONIZATION TECHNIQUES FOR ME
- Page 174:
-U I 1 b I l l . . . . , Figure 2:
- Page 178:
@ & a time acquisition. Due to thc
- Page 182:
6 SYSIXM SYNCHRONIZATION ALGORITHM
- Page 186:
TACSAT payload. Sptinl and time syn
- Page 190:
\ I ..I , .. . . U' c L. rL 50 i !
- Page 194 and 195:
It is IqmmtQlive of the ,wc.sa Cmst
- Page 197:
I' !'.
- Page 201:
v / I ,p ,
- Page 204 and 205:
f I
- Page 209:
3. IAUWCUU SVSTEM SELECTION CRUQTXO
- Page 213:
19-41 5.8.1.8 A/Im faniity of whicl
- Page 219:
CURRLHT PRowcTKm N DEVELOPMENT " P
- Page 223 and 224:
.clrc;lih w m iua thc orhilot planc
- Page 225:
19-10 OcazO midm ~ r nof mp htb~rm
- Page 229:
19-12 0 'I% whicles must PW: lnunch
- Page 233:
8.3 Uniad KingdodWussia Inrtn'm HOT
- Page 237:
1P.16 'II-tcx chen@ngcnvimnmcntal c
- Page 241:
SPACECRAIT AND I.AIJNCII SIISlT.MS
- Page 245: c Firvn 4. Horimld vrhiclr andpaylo
- Page 248: H 8p~nwmd by DARPA ud will dcliwr8
- Page 254: 'ThcTauNt prylodckcoicwl inlnlactt
- Page 257: 20-10 (hcntercoaunnndma have ben di
- Page 261: RESUME Puisque ks futun lanceun per
- Page 265: . 232 CdcJ du IIIOIWYHI?~ Mmoeuvm m
- Page 269: En rcvnnchc, m ce qui concemc la pe
- Page 273: 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 303: 12-11 Spacecraft Family Carrying Ty
- Page 307: 23-2 . - missile wnrninq, e.g. agai
- Page 311: 234 L -'*. f . . 23 AOCS Opntioncrl
- Page 314: i3-6 yuratiori. Whcel desaturatioo
- Page 318: 23-8 tional and storzge capacity aa
- Page 323: contains thc H/w systcm configurati
- Page 327: Figs. 2.1- la-2.1- IC: Parmeters fo
- 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
- Page 371:
i 0
- Page 376:
I 0 I I I @. I 1 @uc?otion: You men
- Page 380:
aLRaqy1 rsmnto ,.verviaw An incrooa
- Page 384:
264 giving tho nunbor of oaeollitnn
- Page 387 and 388:
0 I
- Page 390:
280 65.0 63:6 40.1 360 84.6 81.8 56
- Page 393 and 394:
I I I
- Page 395 and 396:
I I I
- Page 398 and 399:
The small size aaad low mts of the
- Page 400 and 401:
The dediated nature of the sumeiUUa
- Page 402:
274 The outhe cdmcept of a SAR moun
- Page 406:
In order to erform a useful recoanw
- Page 409 and 410:
I I
- Page 411 and 412:
-.- I I I I I !
- Page 414:
27-10 Currcunaly available ground a
- Page 417 and 418:
I ! I I I I I
- Page 420:
Figure 1 Figure 2 \ '. 0 # --e- I i
- Page 424:
SliMMARY Cost and ycrformancc techn
- 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
- Page 470:
, I I I : I I 33-4 . I. psitiom am
- Page 474:
Figure1 World Met roroloKy -h Visib
- Page 477:
, Comment: TACSATS, 1 only as "truc
- Page 481:
. 1.