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Payload spin assembly for the commercial Titan launch vehicleA contract was completed to design, build, and test a Payload Spin Assembly (PSA) for installation onto the Martin Marietta Titan 3 Commercial launch vehicle. This assembly provides launch support for satellite payloads up to 5783 kilograms (6.37 tons) and controls release, spin-up, and final separation of the satellite from the second stage. Once separated, the satellite's Perigee Kick Motor (PKM) boosts the satellite into its transfer orbit. The first successful flight occurred December 31, 1989. Requirements, design, test, and problems associated with this mechanical assembly are discussed.
Document ID
19910015307
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Robinson, Wilf
(Honeywell, Inc., Glendale AZ., United States)
Pech, Greg
(Martin Marietta Corp. Denver, CO., United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1991
Publication Information
Publication: JPL, The 25th Aerospace Mechanisms Symposium
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
91N24621
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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