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Development of the Toggle Deployment MechanismThe Toggle Deployment Mechanism (TDM) is a two fault tolerant, single point, low shock pyro/mechanical releasing device. Many forms of releasing are single fault tolerant and involve breaking of primary structure. Other releasing mechanisms, that do not break primary structure, are only pyrotechnically redundant and not mechanically redundant. The TDM contains 3 independent pyro actuators, and only one of the 3 is required for release. The 2 separating members in the TDM are held together by a toggle that is a cylindrical stem with a larger diameter spherical shape on the top and flares out in a conical shape at the bottom. The spherical end of the toggle sits in a socket with the top assembly and the bottom is held down by 3 pins or hooks equally spaced around the conical shaped end. Each of the TDM's 3 independent actuators shares a third of the separating load and does not require as much pyrotechnic energy as many single fault tolerant actuators. Other single separating actuators, i.e., separating nuts or pin pullers, have the pyrotechnic energy releasing the entire preload holding the separating members together. Two types of TDM's ,described in this paper, release the toggle with pin pullers, and the third TDM releases the toggle with hooks. Each design has different advantages and disadvantages. This paper describes the TDM's construction and testing up to the summer of 1993.
Document ID
19960020698
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Brown, Christopher W.
(NASA Johnson Space Center Houston, TX United States)
Date Acquired
August 17, 2013
Publication Date
February 1, 1994
Publication Information
Publication: The 2nd NASA Aerospace Pyrotechnic Systems Workshop
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
96N24221
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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