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OI~UI'IS MISSIONS I PAYLOAD TYPE -.- DUS PARAMETERS GNBC Stabilization SIC Puiiitiiig ( SWXJ cycles) cS001yr Stressing < 50 PPM 01.1 1131 COMM (I IIMJ mi) NAVIGATION 3-arir .5 tu .I .5 10.02 Noiic s. L, u111: 4Kbp c 10.6 Iiitcniiillciit NU I no Yo (+. .lOdcg) No No Ycs 5 M I yr Mud io low < 50 PPM - -- GEOSY NCIIIUlNOUS EAHTl I OHUITS ELECIHO . COMM 01'11 CA L 3-axis .l to .U1 .I lO.oo01 Nunc X. SIIF. U1F up to 274 Mbps
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 47: e lDiscussiopa Question: To meet st
Page 51: 0 e t 1. ..- .. ' I I t I ' .I... .
Page 55: 0 4-4 Ref 2 Lyon K G and M R Willnr
Page 59: 44 Annex p1 Optical system B. 1 Bac
Page 63: TACSAT @mognd ColpflmU anad Data Co
Page 67: &ring the full novel TACSAT mission
Page 71: authorities have confirmed that TAC
Page 75: TACSAT-SPACECRAFT BUS CONCEPT AND D
Page 79: only bccomc pcrtincnt if vcry cheap
Page 83 and 84: 'DES CROS SATELLITES EN NOMIIRE LIM
Page 85: 0 0 - les mtmoires de massc .. les
Page 89: I I) U-8 certain nombre d’outils
Page 93: n-tu T~RUSlER :61 PUOPELLANI IANK (
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10-2 instant donnt, il put dtlcnnin
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ploccr sur nrhite In n ihc masse fi
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0 10-6 Ccst dans ce COS que le volc
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10-11 I,'nnolysc du coot de meintic
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10-10 Discussion Question: Please p
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11-2 b. m All thc air opcntions USC
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11-4 TACTICAL SATELLEES FOR AIR COM
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11-6 !' i i [XCSATS FOR RESOURCES M
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11-8 I OPERATIONAL IMPROVEMENTS FOR
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CONSIDER4TIONS FOR NATO SATELLXE CO
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It should be noted that the data in
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RX de hop a) Non-lransparent satell
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0. l 6 Table -2 (a) System Evaluati
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ADVANCED TECMNOILOGIIES FOW LIGHTWE
Page 158:
0 a ACKNOWLEDCEMENTS The concepts w
Page 162:
I P\'~'~~~IzER PHASE IG TRhNSIENT (
Page 165:
0- PREPROC PREPROC i 16 COMMUI(ICAT
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MULTIPLE FUNCTION AJ PAYLOADS Figur
Page 172:
e muior, MDR ryp &U nier up Io ud i
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.. 0 sdcly assumed In either of thc
Page 180:
e 174 in which P- is tk prabrbility
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17-11 . IO" . . IO' 0 2 4 6 8 10 12
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, 1 SURUMARY Thispa~rc:.amincscanmu
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4fi 2345 hm 0830 hrs' 2245 hrs 270.
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Flg. 4. Mmpd 8 d Rock, WA. -17-16-$
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C. c 1-- 24 U < L c 0 - c i C - ,9
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6x1 Cammm To mqienasclz: 1 P 4 lln
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0 0 18-1 1 (91 Mayes. d&ri D.. Dycr
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mum (3 ~qnrlra;Og~m.or~~~n.olR6r?Qi
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1 6.1 Cumt ud NcwTcm, r*n.ri and Pr
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6.2.2 UniEcd Kin~domlNonvay I-ii~lc
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7.9 Fmmp 1.9.1 Unitrd Kingdom (U0 M
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Many of thnw splcms and platforms w
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25.. NFQ %&myr* Spcrcc Clipper. Cam
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Figvn 1. Pegorus kjligh. 1
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Wilbpflamed pailbnin6ofrrbkk1mdfril
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payload upruiun syucm is availnhle.
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APEX 1993 247 kg 375w 3 Axis, 0.5'
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countries for several years. Couple
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21-2 2 POSI'6"ION DU PROBLEME 2.1 M
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214 Dens le cas ."un aanslen bi-imp
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21-6 ,...-. ".._ . + . I.. 0 8 IO I
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21-8 Cea finurea montrant qul le co
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21-10 d'iugrnmter nu cours des itdr
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I - - AI with Ihr cue of LOSAT-X. O
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Thc ADACS provido *ti!dc &lamhh ud
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.- I
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12-11 Spacecraft Family Carrying Ty
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23-2 . - missile wnrninq, e.g. agai
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234 L -'*. f . . 23 AOCS Opntioncrl
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i3-6 yuratiori. Whcel desaturatioo
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23-8 tional and storzge capacity aa
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contains thc H/w systcm configurati
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Figs. 2.1- la-2.1- IC: Parmeters fo
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Fig. 4.1-1 a/h: SIC orientation U2
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4 2 0 -2 -4 t . . . I "W Fig. 4.4-1
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Control Accuracy 1 Control oncep pi
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0.75 - 0.2 2 - 0.6 6 - 1.85 IO - 3
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abic 4.2-2: Corrcspadaucc bcwccn to
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lpnpQR rOYi0WS the QdVOUItQ~OQ and
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3.2 P A tuimira ~ ok c~,~~a~aellona
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Thoro are sovoral additlonal positi
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- it is possible to use 8 low level
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I . Ihfcmc Advanced RcJcuch hojccts
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- physical and mvirnnmmtal rrquirem
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IMPACT rill work cbuly wilh thr MIL
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i 0
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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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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
Page 481:
. 1.
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