- 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 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 329:
23-14 e I w 11 n IS n n a 41 U 9s M
- Page 332 and 333:
23-16 / Fig. 4.3.1: ICDS principle
- Page 335:
23-18 Communication Weat her - Oper
- Page 339:
23-20 r - .-_ -- - -. --_.._ I U i
- Page 343:
23-22 I .a * .o.s 8.2 am3 c 0.012 a
- Page 347:
PRW mrms lottrfrsa : UDir Bnterfscc
- Page 351 and 352:
24.2 CJ6Qh ion pl'b;pPelaion tho ap
- Page 353 and 354:
48 iao 4.b 11 8.2 19.3 26.5 88.6 C
- Page 355 and 356:
I I ! I i ~ I I I I I I I ! I I I I
- Page 357 and 358:
[ Z ] C. Purrotta, M.Bieconi, A. Bi
- Page 359 and 360:
I 23-2 2. ):SADLISG TF.CIISOLOGY PR
- Page 362:
124.1 PhwdAwmy Mimv.~tnhbkL.u#eApn(
- Page 366:
Lulrhd durimilr NASA md Navy p*bd o
- Page 370 and 371:
2s-a The paylord concept is distinc
- Page 374: 2s-10 \ I i I f
- 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
- Page 399 and 400: ! I I I
- 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
- Page 422: 27-14 , I I
- 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.