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Miniature Release Mechanism or Diminutive Assembly for Nanosatellite Deployables (DANY)Miniature release mechanisms constrain objects, such as deployables during the launch of space vehicles, such as small satellites and nanosatellites, and enable the release of the objects once a desired destination is reached by the space vehicle. Constraint and release of the objects are achieved by providing a secure threaded interface that may be released by the release mechanisms. The release mechanisms include a housing structure; a release block can include a threaded interface; one or more retracting pins; one or more release springs; a breakable link, such as a plastic link; a cable harness clamp; and a circuit board. The release mechanism can be 0.1875 inches (approximately 4.8 mm) thick.
Document ID
20170001254
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Santos Soto, Luis H.
Hesh, Scott V.
Hudeck, John D.
Date Acquired
February 3, 2017
Publication Date
January 17, 2017
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
Patent Number: US-Patent-9,546,008
Patent Application Number: US-Patent-Appl-SN-14/501,724
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,546,008
Patent Application
US-Patent-Appl-SN-14/501,724
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