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Caging System for Drag-free Satellites

Completed TRL 6 (started at 4, targeting 6)

Description

Next generation drag-free space systems will provide autonomous precision orbit determination, more accurately map the static and time varying components of Earth's mass distribution, aid in our understanding of the fundamental force of gravity, and ultimately open up a new window to our universe through the detection and observation of gravitational waves. At the heart of this technology is a gravitational reference sensor, which contains and shields a free-floating test mass from all non-gravitational forces. A caging mechanism is used to mechanically secure the test mass during launch and release it with a low relative velocity once the satellite reaches its designated orbit. The test mass dynamics during the uncaging process can’t be studied in a laboratory environment. We plan to use the parabolic flight opportunity to test the caging mechanism in a zero-g environment and acquire data to analyze the test mass dynamics.

Benefits

Potential users are NASA’s Earth Sciences Division, the Earth Science Technology Office, and Physics of the Cosmos program

Details

Technology areaSensors and Instruments > Remote Sensing Instruments and Sensors > Detectors and Focal Planes
ProgramFlight Opportunities (FO)
Lead organizationStanford University, Stanford, CA
Start date2013-04-16
End date2016-04-16

Project contacts

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How to get involved

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