Payload spin assembly for the commercial Titan launch vehicle

Details Payload spin assembly for the commercial Titan launch vehicle Payload spin assembly for the commercial Titan launch vehicle

May 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991aeme.symp..253r&link_type=abstract

In JPL, The 25th Aerospace Mechanisms Symposium p 253-274 (SEE N91-24603 16-39)

Physics

Interfaces, Payloads, Spacecraft Launching, Spin Stabilization, Structural Design, Titan 3 Launch Vehicle, Acceleration (Physics), Installing, Perigees, Transfer Orbits

Scientific paper

A 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.

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