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Apparatus for retaining and releasing a payloadAn apparatus for latching an object, such as a payload for a space vehicle, includes an expandible latch which is shifted between a relaxed open condition and a flexed closed condition by actuation of a pair of temperature-responsive members, such as shaped memory alloy (SMA) coil springs. One of the two temperature-responsive members biases an actuator into a first position that allows the expandible latch to open. The other SMA member biases the actuator in the opposite position to close the expandible latch. Heating the appropriate SMA member causes the actuator to move from one position to the other position. In the preferred embodiment, no power is required to maintain the actuator in either position once the position has been established. For example, the actuator may have a rest position that allows the expandible latch to remain open when the two SMA members are cooled and allowed to reach an equilibrium condition with respect to applied force to the actuator. A detent-and-ball arrangement may be used to maintain the position of the actuator after the expandible latch has been closed.
Document ID
20080004033
Acquisition Source
Goddard Space Flight Center
Document Type
Other - Patent
Authors
Carrier, Alain
Cobb, Bruce
Date Acquired
August 24, 2013
Publication Date
October 3, 2000
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-781359
Patent Number: US-PATENT-6,126,115
Funding Number(s)
CONTRACT_GRANT: NAS530682
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-6,126,115
Patent Application
US-PATENT-APPL-SN-781359
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