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These arc three spccific fecornmen&tiom: (1) These papers should be uscd as thc foundation for Ihc Working Group 16 cffw. (2) Thc rcsulrr. of Working Group 16 should lhcn be bricfcd lo mcrnbcr nations and NATO hcadquarlcrs. (3) A NA'J0,min s~uld bc cslablishcd IO drvclop tcchnical and opcrationai options, with costs. to be rcportCa out lo NATO by early 1994.
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 31: ABSTRACT The concept of a Tactical
Page 35: capability bought, the higher the c
Page 39: these parameters vary both as funct
Page 43: Theater Mission Surveillance Orbit,
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
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only bccomc pcrtincnt if vcry cheap
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'DES CROS SATELLITES EN NOMIIRE LIM
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0 0 - les mtmoires de massc .. les
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I I) U-8 certain nombre d’outils
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n-tu T~RUSlER :61 PUOPELLANI IANK (
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I. !. I. ...... . .... ...... .....
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! ' ' I' I ';, . ..
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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
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0 a ACKNOWLEDCEMENTS The concepts w
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I P\'~'~~~IzER PHASE IG TRhNSIENT (
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0- PREPROC PREPROC i 16 COMMUI(ICAT
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MULTIPLE FUNCTION AJ PAYLOADS Figur
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e muior, MDR ryp &U nier up Io ud i
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.. 0 sdcly assumed In either of thc
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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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- .d: 5.1.2 EMlOP Eump is Pcpn:scnt
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1 6.1 Cumt ud NcwTcm, r*n.ri and Pr
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0 0
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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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! --- ----FE- UICLIEASWO SAIEI Ill
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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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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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