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6.2.2 UniEcd Kin~domlNonvay<br />
I-ii~lc lmimkrfor Low Emh Orbit (l.iiil.k'O}. '?k mm mcrcia1<br />
IittIXQ program is king undcrtakcn FpII GcRc~;~~ 'lcchnology<br />
Sptems Ltd and the NorwqianSp,?rrj: Ccntcr(Norok<br />
Romwntcr) to offcr a kwarrt and mlinhk n,cnnn of plasina<br />
small p3yln-A~ into hmth polar and sun-oynshrnnrws orhits<br />
from a Eumpctcn launch sitc. l'hc ljttl .EO i7 m wlid propellant<br />
vchEck:copnhlcofpliccinan 1,3~Ih((~hn)payIontl into<br />
a 243 nm (052) km) pilar orhit or 1547 19, (1d3 kc) i 110 a<br />
162 nm (3w) hm) polar orbit. It wuld trc 1aursI)cd froin the<br />
Andoya Wmftct RmRc (69 dcg 17 min M. 16 ckg 01 min E)<br />
Morc than rlM) souding rtrkcts hnvc hrcn I~i~rrchsd from<br />
this titc. littl.EO aiuY atso inr;;..fh 2.m Ih (312 kg) into a<br />
162 nm (SM) km) polar orhit fmm Itbly's San Mnrco launch<br />
site.<br />
6.2.3 Spin<br />
I<br />
C~pricomi~. Thc lnstituto Nacional Dc Tccnica Ac.rtap;tcinl<br />
(INI'A) has annnunccd a ncw rtrkcl &vclopmcnl. thc<br />
Caprimrnb. which is intcndcd to prodc Icw-cmt spm<br />
transportation for thc scicnlific and communicritions community.<br />
It is a Ihrcc-stagc all-sdid rnckct c:tpnb!s of placing<br />
I10 to 228 Ib(M to IOkg) into a 324 nm ((100 kti:)p)lnrorbit.<br />
Tcsu dl ttc mnductcd from El Arcncnilb (iluclm), a d<br />
thcrc arc plans lo build a future launch cnmplcx in thc<br />
Canary Islands.<br />
I<br />
6.2.4 Comnmtru~rulth of Indrprndrni Siatts (CIS)<br />
Spacc Clipper. Yuzhmyc NPO. bawd in the Ukraine, is proping<br />
an air-lnunchcdcnmmcrciill Iilunch Rystcm.spna.clip<br />
pcr. which is planned to hc availnhlc in 1W4. Thc srtcm<br />
cnnsists of an An-I24 canicr aircrdft and a chriicc ofscvcral<br />
thrcc- or four-stagc solid propellant launch whiclcr(krivcd<br />
from the SS-24 misdc) that arc launched from tl~c cargo hay<br />
nfthchn-124. Achoiccofsudiffcrcn1u)lid rmkct launchcm<br />
has bccn propcncd. 'I'hc b,wlinc systcm in cnpnhlc ofdclivcrina<br />
1,Iall Ih (500 kg) to I.EO and is mtdulori7rd to pttwidr<br />
six diffcrcnt wninns of thc vc!wlc ;Ind dapt In a wkk variety<br />
of orbital recpircmenu. Thc maximum tnlrcoff wight is<br />
392 tonnes. and the systcm is claimed to b phfr to opcratc<br />
from any sirftcld capabk ofscrvicing a ?kin3 747. 'ki avoid<br />
techmlolSy transfer reotrictions. thc inntnllafkin of the paykx4<br />
can bc ptrfwrr~ed on-bird the Antomot t k cu~tomer's<br />
eirftehs. Yuzhnoye plans to mcnlify two An-la aircroft,<br />
and them are more than 100 SS-tas in Inwntary. It Lo<br />
WACE CUPPEW (CIS)<br />
F M 0. Ab-- WlW Leunch Wkh<br />
19-11<br />
7. ~U.U.US'ITU@ MDSSOI&DKW'JVED IAWNCH<br />
RVSPlEMS<br />
l$S a mull of IDCe lJSlC9S Stratcgic Arms Hcduction Talks<br />
(START) a&rcemcnls. tk use of surplus stratcgic hallistic<br />
missiles for launchin8 12lsa(s nccds to be mnsidercd. Thcrc<br />
are. ofcou~. many ixsucs that must he addrcsscd in dctcrmininB<br />
thc prRcticiility and advantagcs of this option. Thc<br />
fixtors includr thr latcst trcnds in the arms rcduction talks in<br />
termsofdctcrmining thc Iyp and numhn of strategic bnl-<br />
Iistk mi%rilcs that might kccomc availablc and ;my trcaty<br />
rcslriclionson tkirulc twspacc Iaunchcn: the p;iyloidcapi\hility<br />
to typical orbits of intcrcst and thc payload mmp:irtmcnl<br />
dimensions; and cstimatcs of thc non-rccurring and<br />
rccurrina mls. With rcqxct lo Iiiunch rcspmsivcncss, thc<br />
1and-h.wi ballistic miuilc on alcrt status rcprcwnts thc ultimarc.<br />
with rcspnsc timcs in thc onlcr of rconds. 'I'hc cost<br />
and othcr issucs rclatcd to maintaining this typc of caphilit)<br />
prcrnls the limiling c;w of launch rcsp)nsivcncss.<br />
Thc trcnd in thc strategic nuclciir wrhcad rcduction tiilks is<br />
forbnth thc IJSand IhcCIS togo in twophnwsfrom thccur-<br />
rcnt total count for all thrcc Icg of thc Triad of somewhat<br />
mom than IO.QM) warhcads to 3.(MTr3.50 wirhcads by thc<br />
ycar Mn3. Thc first p hw rcduccs thc total numhcr of wilr-<br />
hcads lo 3,MO-4.2%1 in svcn ycars or lcxr from thc cxccu-<br />
lion datc of the trciity. Within thw ovcrall Triad limits.<br />
thcrc arc spccific 1imitsplacc.d on the Intcrcontincnlal nallis-<br />
tic Misilc (ICHM) and Ea launched Ilallistic Missilc<br />
(SI.IPM) forces. At Ihc cnd of the first phase. thc numhcrof<br />
ICIHWs cannot cxcccd 1.2tIO. and thc numhcr of SI.nMs can-<br />
mit cxucd 2161); for thc sscond ph,w 1hc.w limits arc 1.200<br />
and 1.756). rcspctivcly. In thc sccond phwc thcrc is illso a<br />
rcquircmcnt that all thc rcmaining ICHMs cnrty only one<br />
warhcad cach. whilc thc SLIMS can mntinuc toc:irty multi-<br />
plc warhcads.<br />
7.1 United Slates<br />
Within thc limiuoutlincd abvc. thcrc arc still n largc numk<br />
r ofpruiblc distrihutionsofspccific misdc rctluctions and<br />
thcrcforc of their availability for space launch. tlcnvcvcr. TA<br />
far (09 lis missilcs arc mnccrncd. 'lkhlc 3 show n gcncrally<br />
scocptcd rctircmcnt schcdule and indicatcs that. hctwcn<br />
m and thc year 2UlXb2bll)3. thc Minutcman lis (MM-11s)<br />
and the Navy W idon C-3 and Widcnt C-4 missilcs will bc<br />
rctimd and may bc available for othcr applications. Aftcr<br />
that time perkd. tk'Rccnty wll rcquirc Pcncckcepcr midcs<br />
8o Rs retircd kauw of NJulltpk Ittdritrndcntly-Tar~ctcd<br />
RcentryVchkk(M1WV) limitations and spccificdc-MIRVing<br />
rub The cx~ct number of Pcscckecpcn that would be