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19-10
OcazO midm ~ r nof mp htb~rm ~ ~
mm thCP FV m&y im jpdudkm imlsdc tlw Bu
SJ:,X &,:ix:; (E'%) Ari:am Tbchpw~
fu4m (MTEP), the F~mh
in t k mmmcrcial
Expriment T 88-
Motre Ponus. the Italian Itabpct-
Micra30t. nnd tk British Univcmity of Sumy UoSat,
hilt by Surrey Sotellik RchnoEogy Ltd.
6.8.2 lgassn
k4-VSok.r. l?te fir01 of tk M Rmily dwhiclcs wrc eitkr
lhm- OP fciur-aoge all moiid-propellQnt whicles msBc use of
mmdyniamk art$ opin-otlabilizotbn oontrol techniques.
Pnicr wmbm U& 1~~08lcliary Cue1 injection for thrust mor control in mpm to an on-board sutogibt. and eventually
tRE edpntml opkm ww di@d to imremc control lq+c
dagn flexibility and to &ucc psurcr ami wight needs. The
cumnt pduabn .wsbn is thL' M-3S-11. wkmecharaacristics
8rc listed in Figure 6
6.U.3 India
SLVSePieJ. The Aupented Spa02 ~ AIJ~C~ Vchicle (ASLV)
can lift 330 Ib (1% ha) into LEO. The launch of thc Polar
Satellitc l ~unth VehCrh (FSlW). planned for March. 1993. is
mpcctcd to &liver 6.6Q1p Ib (3.000 kg) to IEO. The PSW,
unlikc the ASLQ, which is crimped of four .solid slap and
two strapnns. will use liquid sccntxl and fourth stagcs. The
IJS hasplaccdsanctionoonthc IndianSpacc RcscarchOrganintion(9SWO)for
buyingadvanccd mkct vchnology from
Russia. Thecharactcristiaof the Indian vchiclcs arc listcd in
Figure 8.
cuznmn IM DEVELOPMENT
CWCVKm I
Figure 8. Cwml end Planned Indian bunch Systems
6.8.4 isml
Slrcrvit. Thc Shavit (which trandatcs to Comet) is a
threz-ctnp mlko pmpllant vchick and is a mdificntion of
t k Yckb P I Dntcnncdiate Ran@ IBollistic MiKqilc (IRIIM).
Ths Jepicb io claimed to be capable of hunching a MO Ib
(Sm, kg)wnrhccJ. A satellite. Offcq 2. wns launched success-
fully on 1 April. 19%) into an clliptic;ll orbit with a pcrigcc of
12.6 nm (210 hm) an4 an apogee of er#, nm (1.500 km). The
onteliite weimt io estimated to be 352 Ib (160 kg) The LEO
copccity in on eetirnoted 400 Ib (200 kg) into a retmgrade
orbit.