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SI-200 bus system is based on the RazakSAT (aka MACSAT) bus technology, which is being jointly developed with ATSB of Malaysia for its national space program. SI-200 bus is designed for Low Earth Orbit small satellite missions. It can accommodate various kinds of payloads for electro-optical Earth observation, telecommunications, and space science by offering relatively large payload space. This bus system can be flexibly re-configurable to adapt different mission and user requirements. This system is an attractive platform for small satellite missions with the following characteristics:

Compact hexagonal frame structure
Affordable volume and mass for small satellite launchers
Active full 3-axis attitude stabilization
High reliability system with redundant design concept
High speed data downlink capability for complex payloads
2.5m resolution remote sensing payload (MAC) on-board as baseline design
 
Item
Specifications
Remark
--Mass
< 200 kg
 
--Volume
¨ª 1200 x 1200 (mm)
 
--Power Generation
330 W @ EOL
--3 Deployable panels
--Battery
6Ah ¡¿ 3-pack
--NiCd
--Attitude Stabilization
Full 3-Axis
--Zero-momentum
--Pointing accuracy
0.2¡Æ
--3-Axis
--Attitude Knowledge
10 arc sec (1¥ò)
 
--Off-Axis Tilting
¡¾45 deg
 
--TT&C Link
S-band(9.6 / 38.4 kbps)
--FSK
--High Speed Data Link
X-band
--QPSK
--Lifetime
> 3 years