Capabilities
ALL-STAR aspires to deliver a 3U CubeSat with the following specifications:
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Structure:
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Standard 3U CubeSat
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Payload volume approximately 8 x 8 x 16.5 cm
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Payload mass allotted 2kg including payload structure
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ALL-STAR bus can provide payload with a structure or the payload can design their own

- Power:
- 10 W total nominal draw throughout the orbit
- 30 W for 15 min peak
- Payload will have a nominal draw of 4.5W
- Command and Data Handling:
- Handle all subsystem interactions
- Memory storage for payload
- Capable of reading digital and analog sensors from the payload
- Software:
- Modular, easily-changeable for each mission
- Interfaced through a GUI
- Position Knowledge:
- On board GPS
- Accurate to within 100 m in LEO
- COM downlink:
- Minimum of 250 kbps
- Goal of 1 Mbps
- Attitude Knowledge and Pointing:
- Knowledge accurate to within 0.2°
- Pointing accurate to within 1°
- Propulsion:
- Optional module
- ΔV 10 m/s