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Sphere launcherThe sphere launcher was designed to eject a 200 lb, 15 in. diameter sphere from a space vehicle or missile, at a velocity of 58 ft/sec without imparting excessive lateral loads to the vehicle. This launching is accomplished with the vehicle operating in vacuum conditions and under a 9 g acceleration. Two principal elements are used: a high thrust, short burn time rocket motor and two snubbers for reducing the lateral loads to acceptable limits.
Document ID
19720018730
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reed, W. B.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 6, 2013
Publication Date
June 1, 1972
Publication Information
Publication: NASA. Ames Res. Center 6th Aerospace Mech. Symp.
Subject Category
Machine Elements And Processes
Accession Number
72N26380
Funding Number(s)
CONTRACT_GRANT: N00030-68-C-0303
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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