0 - FTP Directory Listing - Nato
0 - FTP Directory Listing - Nato
0 - FTP Directory Listing - Nato
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0<br />
8-4<br />
specific tools for each main arcas of cngincering<br />
design arc shown. They can be concurredy call<br />
on demand by the different experts working in<br />
parallel for trade off or validation on diflcrent<br />
fields : clcctrical, thermal, mechanical , orbit<br />
environment, attitudc and orbit contrbl,<br />
dynamic , propulsion, payload accomodatidn,<br />
mission; satellite programmation, ctc ...<br />
i<br />
Presently, SYSTEMA is uscd primarily in thc<br />
first part of the developmcnt process (fig 4).<br />
from phase A proposals, mission and s.\tclli!c<br />
layout tradc-offs to the end of ph?, * L with<br />
dctailcd satellite design optimisation . VI' up to<br />
proposals for a phase C activity. I<br />
If additional risks causcd by eventual flaws rjr<br />
bugs in numerical simulations arc acccptcd -<br />
these risks arc assumed to bc affordable far<br />
small tactical satellites with not vcly<br />
sophisticatcd missions -, phase C validation tjy<br />
mcans of such concurrcnt engiiieering only tools<br />
would saw not only thc major portion of the<br />
environmcntal tcsts costs (thcrmal, kacuum. suh,<br />
vibrations) but also would rcducc thc schcdulc<br />
induced costs.<br />
Such an approach has dcmonstratcd its<br />
cfficicncy through thc SSOT prograinmc (fig 5).<br />
S80T is a microsatellite launchcd this sunimcr<br />
as a conipanion of TOPEX - POSEIDON<br />
SPACFCRAR on ARIANE. SSOT has<br />
bcncfitcd from an intcnsivc use of SYSTEMA<br />
from thc first stage of dcsign to the dclivcry ;it<br />
the launch sitc. A programme conducted in a<br />
very short timc for a very competitive cost.<br />
I CONCLUSION 1<br />
The approch prcscnted above is far from a<br />
rcvolution. It is only an evolution.<br />
To be efficient suck concurrcnt engineering<br />
tools need to be validatcd and calibrated by<br />
refcrcncc to the data gathered during previous<br />
dcvclopmenl tcsts or during in orbit monitoring<br />
of opcrational spacccrarts. In that sense such an<br />
approach capitaliscs the whole cxpcrience<br />
acquircd by MATRA MARCONI SPACE<br />
through prcvious or currcnt low earth orbit<br />
programmes : SPOT 1,2,3 - ERS 1 and 2,<br />
HELIOS - SPOT 4 and Polar Platform.<br />
The SYSTEM\ usc built-in flexibility givcs thc<br />
opportunity to quickly update a current design<br />
and thus allows to follow cvolutions of<br />
technologics or accomodatc a newly availablc<br />
equipmcnt.<br />
SYSTEMA ;~llows a short rcaction timc and a<br />
quick acconiodntion on the satcllitc as soon as<br />
cmcrging rcquircmcnts arc formulated by the<br />
uscrs.<br />
~ll~iisimiiotts<br />
Jw rhis Seciion appear immediaiely<br />
afim ilte Fmrc~lt mnshiion.)<br />
i.