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Multi-axis Attitude Control and Energy Storage on Small Satellites

Completed TRL 6 (started at 3, targeting 6)

Description

To fully-enable cutting edge science through small satellites (smallsat), this technology will reduce the overall size and net power consumption of conventional three-axis attitude control systems.

A CubeSat is a volume-limited, standardized smallsat form factor (typ. 1-6U, where 1U = 10 cm3) that occasionally needs to be equipped with an active attitude control system, e.g. reaction wheels needed for high-resolution science imaging, orbit maintenance, and maximum irradiance on solar cells. The proposed architecture provides improved performance over traditional wheels and satisfies the push for component miniaturization, increased pointing accuracy, and power efficiency on CubeSats.

Benefits

N/A

Details

Technology areaGN&C > Control Technologies > Control Force and Torque Actuators
ProgramCenter Independent Research & Development: GSFC IRAD (GSFC IRAD)
Lead organizationGoddard Space Flight Center, Greenbelt, MD
Start date2012-10-01
End date2014-09-01

Project contacts

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How to get involved

This is early/mid-stage (TRL 6) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.

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