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Payload Launch Lock MechanismA payload launch lock mechanism includes a base, a preload clamp, a fastener, and a shape memory alloy (SMA) actuator. The preload clamp is configured to releasibly restrain a payload. The fastener extends, along an axis, through the preload clamp and into the base, and supplies a force to the preload clamp sufficient to restrain the payload. The SMA actuator is disposed between the base and the clamp. The SMA actuator is adapted to receive electrical current and is configured, upon receipt of the electrical current, to supply a force that causes the fastener to elongate without fracturing. The preload clamp, in response to the fastener elongation, either rotates or pivots to thereby release the payload.
Document ID
20150003275
Acquisition Source
Goddard Space Flight Center
Document Type
Other - Patent
Authors
Young, Ken
Hindle, Timothy
Date Acquired
March 18, 2015
Publication Date
April 29, 2014
Subject Category
Spacecraft Design, Testing And Performance
Space Transportation And Safety
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-12/940,771
Patent Number: US-Patent-8,708,322
Funding Number(s)
CONTRACT_GRANT: NNG09HR00C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-8,708,322
Patent Application
US-Patent-Appl-SN-12/940,771
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