NASA NTRS · 20160011982
System and Apparatus for Deploying a Satellite
Abstract
A 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.
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Santos, Luis H., Hudeck, John D.. 2016-09-06. System and Apparatus for Deploying a Satellite. https://ntrs.nasa.gov/citations/20160011982
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