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T~RUSlER :61 PUOPELLANI IANK (7)
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Class It multimission spacecraft
CAPABILITY:
SPACECRAFT FEATURES
SUN SENSOR (41
Mission life
3 to 4 years
Orbif altitudes : 200.1000 km
Payload available mass : up to 200 kg
Payload available power : 100 W mean, 200 W peak
Battery capocity : 9or 1BAh
28+/-4V
VakY.
Ani e painling ' ' accuracy : +/- 0.15 deg
Data storage an board : 5 Gigabits
Dolo transmission 2 to 8 Kbits/wc
Encryplian : optional
SATELLITE BUDGETS:
Mass Power
Payload :
Platform : ____
Hydrazine :
( 4 years mission ]
624- ._ . IIOW -.-a. n -
1 BO Kg
8 KCI -
60 Wan
-. .__
Total : 250 Kg 170 Wan
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RF ANTENNA I?)
PAYLOAD MODULE
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L EARTH SENSOR
The FAIRCHILD/MATRA MARCONI SPACE
spacecrah is a light weight, lawcast slructure designed
to accamadate a wide range of scientific and
operational payloads . It provides a simple, efficient
power system with a super-NiCd battery and a
modular solar array thot can be adapted lo various
orbit geometries and payload demands . The central
data processor unit includes an embedded solid-state
recorder and generous margin far growth . The
attitude determination and conlral system and the
propulsion system are bath designed for flexibility
and long life ,