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Gimballing Spacecraft ThrusterA gimballing spacecraft reaction-control-system thruster was developed that consists of a small hydrogen/oxygen-burning rocket engine integrated with a Canfield joint. (Named after its inventor, a Canfield joint is a special gimbal mount that is strong and stable yet allows a wide range of motion.) One especially notable aspect of the design of this thruster is integration, into both the stationary legs and the moving arms of the Canfield joint, of the passages through which the hydrogen and oxygen flow to the engine. The thruster was assembled and subjected to tests in which the engine was successfully fired both with and without motion in the Canfield joint.
Document ID
20100019598
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Pickens, Tim
(Orion Propulsion Madison, AL, United States)
Bossard, John
(Orion Propulsion Madison, AL, United States)
Date Acquired
August 24, 2013
Publication Date
May 1, 2010
Publication Information
Publication: NASA Tech Briefs, May 2010
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MFS-32520-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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