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System and Apparatus for Deploying a SatelliteA frictionless satellite constraint system is provided. The constraint system includes at least one clamp bar configured to restrain a satellite within the constraint system in an axial direction. The constraint system also includes a plurality of pins configured to restrain the satellite within the constraint system in a lateral direction.
Document ID
20160011982
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Santos, Luis H.
Hudeck, John D.
Date Acquired
October 4, 2016
Publication Date
September 6, 2016
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
Patent Number: US-Patent-9,434,486
Patent Application Number: US-Patent-Appl-SN-13/781,121
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,434,486
Patent Application
US-Patent-Appl-SN-13/781,121

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