Hughes Electronics Corporation

Alexander M Benoliel

Vincent E Cascia

Gary J Kayano

A launch lock mechanism having a clamp assembly that secures multiple independent brackets. The brackets are attached to components to be deployed from a satellite. A pyrotechnic separation device actuates the clamp assembly. Both the pyrotechnic device and the clamp assembly remain independent of the brackets and components after deployment.

Independent launch lock mechanism

A friction retaining device for holding and releasing reflector panels of a satellite. The retaining devices having a friction bushing mounted thereon to prevent the reflectors from becoming disengaged from the clamp. The retaining device has a pair of opposing arms having upper ends that communicate with bumpers on the reflectors and lower portions that communicate with a release mechanism. Upon actuation of a pyrotechnic device, the reflectors are deployed. At the same time, the release mechanism disengages the lower portions of the opposing arms allowing them to remove the bumpers from the reflectors.

Growing community of inventors

Redondo Beach, CA, United States of America

Alexander M Benoliel