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Multi-point release mechanismA multi-point release mechanism used on the communications technology satellite. The mechanism is designed to jettison one large panel and to release a second panel; both panels have independent multi-point attachments to the spacecraft and require to be released in sequence. The solar array is stowed concertina fashion under 2 psi pressure to ensure that no movement occurs between the stowed folds of the array during the launch. One pair of linear pyrotechnic-actuators releases both the JBSA and the pressure plate via the release mechanism. This release mechanism has successfully passed qualification level vibration launch and thermal environment tests and has accumulated to date close to 30 successful releases.
Document ID
19740003581
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Groskopfs, E.
(Spar Aerospace Products Ltd. Toronto Ontario, Canada)
Date Acquired
August 7, 2013
Publication Date
October 1, 1973
Publication Information
Publication: NASA. Langley Res. Center The 8th Aerospace Mech. Symp.
Subject Category
Machine Elements And Processes
Accession Number
74N11694
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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