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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

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