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8.3 Uniad KingdodWussia<br />
Inrtn'm HOTOI,. A joint Ilritish/Husvan dcwlopmcnt to fly<br />
an intcrim wnion of thc Ilritith HOTOI. on thc Husian<br />
Antom-225 'MPIR" hcavy lift aircraft is undcmy. Sumssful<br />
wind-tunnel tats at simulatctl spec& of Mach 10.5 a d<br />
14 have ken conducted at the Ccntral kmhylrdynamio<br />
institute(%AGl)in theirT-128wind tunml in [Wmtaw. The<br />
three orpni7~tions haw signed agrccmenu among thcm-<br />
sclva (ps wll as with #heir respectin: gmmmcnt.. . nritish<br />
htmsyax is defining the Acmpaceplanc and airhnrnc<br />
supprl systems. Ijmitcd TCSOUT~: are awilahk. but the<br />
Eumpe~nCommunityCom~:,ission hasbtcn appmhcd by<br />
British Acmpace for support sine the commission has said<br />
it WM entertain joint Europcan6ovkt (now CIS) BCW<br />
space nntum.<br />
Thc vchkk is planncd to carry a paybad of 15.400 to<br />
17.600 Ib (7.OOlJ to 8.0 kg) into IEO aftcr king launched<br />
from thc An-225 at an altitude of abut 28m It (U km) Tk<br />
An-225 quires the addition of tvm extra .%het D-18<br />
engines. Rolh Roya replacement cn@m 6xrc cnnsideml<br />
to amid installhg additional engines but wm rejected am not<br />
R ccgteffcctin' modificatbn. l'hc cnnacpt is illustmted in<br />
Figure 12<br />
8.4 Wosr<br />
Thc assViet Uninn has cnnCucted aidvamrd partia!ly and<br />
fully hllashk nhick rcsearch and testing Urn many yeam In<br />
Nonmtur. 1991. for instance. thr Centml Imtitute of Aviation<br />
Moton. M-,d.ims to haw anr~ucaed the nnt test<br />
9. RAUN6w 911w: WSODERATUOWS<br />
The orbit quimmcnts for thc GEQ and [EO missions discus&<br />
carlkr an h mct by laumhinp fmm thc tw main<br />
launch sites in t k US, Cap Canaverid in Florida. end Van-<br />
3tnBsrg in California Fipm I3 ss#pcm tht orbit inclinations<br />
that ire ahkmblt hm eesh of thz two sitcs. All targcts at<br />
irrclinat~mo~aaaltoorftrothen573tgcanhc rcached from<br />
Cape Cenowml. whik ik hiBkr inclination orbits , includingpolar<br />
end oasn-smhmr#rus. are r;awsibk from Vandcn-<br />
FQm 12. 'bicumm3rc?tOalo<br />
ZzgcZtm<br />
bcr&Tktc Atlrrcrorklte bnatcnvmld launch the GEOsatcliiics<br />
due easi a t of Cepe Cannwml. while sinek I.EO<br />
I<br />
0.2.2 United Kingdm !<br />
satcllita could k laumkd on tk small launch which or<br />
hllistk mksikdcrivaticncs fmn either launch site. large<br />
Monmld Tdit-Qfl and landing (IIOT(Pl.). 'I'hc original<br />
mu'!i-satcllitc c~nstcllat~ns. such as Iridium-litc amcepts<br />
ambitious BBOTOL gqram is currently unfumlcd. The<br />
cnuM bc launckd by hlta or Atlas II out of Vandenberg.<br />
cnginc mmpt for tht )POTOl.&vclqd artd patcntcd by<br />
An Atlas I1 pid is kingbuilt at Vandcnbcrg. For the ballistic<br />
Alan hd ha ken dcclauifikd. but th !%olbRoycc<br />
missik4cr;vintives. thc launch sitc at Capc Canaveral wukl<br />
RWSO hi3n is still kld pmpiictnrg.. Ilk enair# is a<br />
haw to br re-activated. and dcdicetcd launch sites would<br />
preumhd. air-hrenthing mckct that utikm air cntcring<br />
nccd to he atahlished at Vandcnhcrg. Th: cstimatcd<br />
thrtwgh B V-rvnlgcd intake. Thc air isskEDTd drm t05uh<br />
a t for an akovc-grwnd hallistic misilc4crivativc spacc<br />
wnic spx& and p a ! through R rrfts d kilt pchanwn<br />
launchcr pd is about DSM. Thc air-mobilc Pcgm~s offcn<br />
and turkmmprcss4m until it reachcs rcrthet chamhcr prcslaunch<br />
platform survivability and thr maximum flcxibility in<br />
sum liquid h,vdnqcn and liquif6d air Pucl the fiat phmof<br />
launch sitc location and omit inclination. An advantagc of<br />
cnaintflinhtuptoIW~hS.5at nnahitudxoI93.4M)It (Mkm)<br />
the Bcga.tus i+ that for target nrc,w et latitudcs hwr than the<br />
Onbd liquid oxygcn and hydrn@n is U& for the rcmein-<br />
28 dcg of Cap Canaveral. launching at inclinations equal to<br />
der of the flight. HOTOLsharcs icchnn!qp ntcds with thc<br />
thc targct latitudc provides an orbit that alltnw thc satellite<br />
US NASP but its future is unoertain. It is illustrated in<br />
I<br />
more mnxcutive p,wcs m r thc targct than thc two tima<br />
Figure 11.<br />
pcr day achievablc if it were launchcd from Cape Canawral.<br />
It should bc noted that a cost penalty is incurred to exploit<br />
this advantage.<br />
'lihlc 4 lists the mrdinatcs nf mint of thc spacc launch si:cs<br />
that mist (or in some cam arc planned or arc inactin:) in the<br />
wrld. and Figure 14 s b their distrihution. The fluid<br />
global environment that is bund to exist in the future and<br />
thc fa0 that tscsat mision will moat likely be multinational<br />
in naturc (end pcrhap a UN responsibility) rcquire thc mnsickration<br />
of sharing launch facilities. The Italian sitc at San<br />
Marax. off tk mt of Kenya. thc French siie i ~t Kourou.<br />
Frcnch Guiana. and the nrazilian sitc at Alcantara arc intcrcstingbccause<br />
they affod thedircct launch inclinationorbits<br />
for h r latitude targcts. The mlocatablc laurus wuld be a<br />
candidate for using non-IJS launch sitcs but. again. a<br />
custtffectinncu analyxis would need to bc carricd out. The<br />
US. Pcgasus. ',he propd CIS Spacc Clipper commercial<br />
orbital injcction sptcm. thc lJWCIS Interim HOTOL, and<br />
the German Sangcr could also bc launchcd from multiple<br />
launch sites<br />
IQ. @ONCI~USBONS/WF~OMM&NDATIONS<br />
While it is ncrt to impamihlc to predict with ccrlainty the<br />
environment oP thc future and what peacckecping mililnry<br />
capability will be demanded in that environment , thcre are<br />
some things that. in the long-term, appear incvitabk:<br />
There will k a pmlileration of high technology weapon<br />
spa(cm5 mnd thc world in thc hands of nntionatntes<br />
that hiuf no( prcvbusly had aaxm to such wapons.