Satrec Initiative (SATRECI): SI-300 (original) (raw)
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DubaiSat 2 [Satrec Initiative]
SI-300 is the extended version of the SI-200 platform which has flight heritage from RazakSAT of Malaysia and DubaiSAT-1 of UAE. Its architecture is designed to accommodate an Earth observation and/or science payload. Hall Effect Propulsion System (HEPS) is installed for orbit control and maintenance. Accurate and agile three-axis attitude control supports precise imaging operations. Dual redundancies are adapted where necessary in the system architecture design to increase reliability of the satellite system.
SI-300 platform, whose size is 1.5 m in diameter and 1.95 m in height, features deck-and-longeron type structure permitting easy assembly and disassembly. Li-ion Battery and four deployable solar panels are equipped for power supply. The interface with the launch vehicle is made through an adapter bolted to the bottom of the structure.
| Satellite | Ordered | Date | Launcher | Weight (kg) | Remarks |
|---|---|---|---|---|---|
| Launch | BOL | ||||
| Deimos 2 → GEOSAT 2 | 19.06.2014 | Dnepr | 310 | ||
| Dubaisat 2 | 21.11.2013 | Dnepr | 300 | ||
| KhalifaSat (ex Dubaisat 3) | 2013 | 2018 | H-2A-202 | 350 |
Further Satrec Initiative satellite busses: