Capabilities

ALL-STAR aspires to deliver a 3U CubeSat with the following specifications:

  • Structure:

    • Standard 3U CubeSat

    • Payload volume approximately 8 x 8 x 16.5 cm

    • Payload mass allotted 2kg including payload structure

    • ALL-STAR bus can provide payload with a structure or the payload can design their own

Deployment_Structure

  • 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
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