ASI, the Italian Space Agency, is going to finance a developing of a small
satellite platforms production line called PRIMA (Piattaforma Riconfigurabi
le Italiana Multi-Applicativa) with Alenia Aerospazio partnership as Prime
Contractor and sub-contractors preferably chosen within the Italian Space I
ndustries. The main objective of the program is to develop a multi-mission,
easily adaptable Platform for LEO orbits, allowing rapid, efficient and lo
w cost bus for applicative and scientific missions.
The Italian national space plan foresees for the enf of 2001 the build up o
f the Skymed/Cosmo constellation as applicative Earth observation program p
lus a number of small scientific spacecraft with a rate of 2 missions each
three years. To fulfil these schedules, the PRIMA platform should complete
its development and qualification program in order to be ready for the firs
t unit (proto-qualification flight) to interface the first payload (Science
or Applicative).
The intrinsic modularity of PRIMA should allow it to adapt itself to a larg
e variety of missions in LEO orbits with minor modifications. The design wi
ll be conducted in order to get an advanced Platform able to meet a large s
et of missions, payloads and launcher specifications. The platform will be
completed by a ground control centre adapted to the monitoring of PRIMA bas
ed satellites. PRIMA thus offers a very attractive alternative to large-sca
le missions in terms of costs and completion time.
The paper will describe the technical aspects of PRIMA Platform, with parti
cular emphasis put onto its flexibility and reconfigurability for different
missions. The System and S/S architectures will also be presented and defi
ned in view of selected mission cases.
The AIV / AIT aspects will be discussed, with a discussion of the applicabi
lity of Globalstar(TM) approaches, facility and heritage.
Finally, a brief overview of PRIMA first applications /SkyMed/COSMO and Dav
id) will be given. (C) 2000 Published by Elsevier Science Ltd. All rights r
eserved.