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Deployment Mechanism for the Space Technology 5 Micro SatelliteSpace Technology 5 (ST5) is a technology mission that will send three spin-stabilized, 25-kg satellites into a highly elliptical Earth orbit. Each of these satellites must be deployed separately from the same launch vehicle with a spin rate of 3.4 rad/s (32.4 rpm). Because of the satellite's small size and the requirement to achieve its mission spin rate on deploy, typical spin table, pyrotechnic deployment devices or spin up thrusters could not be used. Instead, this new mechanism design employs a 'Frisbee' spin up strategy with a shape memory alloy actuated Pinpuller to deploy each satellite. The mechanism has undergone several design and test iterations and has been successfully qualified for flight.
Document ID
20040084297
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Rossoni, Peter
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Cooperrider, Caner
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Durback, Gerard
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 7, 2013
Publication Date
May 1, 2004
Publication Information
Publication: 37th Aerospace Mechanisms Symposium
Subject Category
Spacecraft Design, Testing And Performance
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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