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Pyrotechnic Actuator for Retracting Tubes Between MSL SubsystemsAn apparatus, denoted the "retractuator" (a contraction of "retracting actuator"), was designed to help ensure clean separation between the cruise stage and the entry-vehicle subsystem of the Mars Science Laboratory (MSL) mission. The retractuator or an equivalent mechanism is needed because of tubes that (1) transport a heat-transfer fluid between the stages during flight and (2) are cut immediately prior to separation of the stages retractuator. The role of the retractuator is to retract the tubes, after they are cut and before separation of the subsystem, so that cut ends of the tubes do not damage thermal-protection coats on the entry vehicle and do not contribute to uncertainty of drag and consequent uncertainty in separation velocity.
Document ID
20100042212
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other - NASA Tech Brief
Authors
Gallon, John C.
(California Inst. of Tech. Pasadena, CA, United States)
Webster, Richard G.
(California Inst. of Tech. Pasadena, CA, United States)
Patterson, Keith D.
(California Inst. of Tech. Pasadena, CA, United States)
Orzewalla, Matthew A.
(California Inst. of Tech. Pasadena, CA, United States)
Roberts, Eric T.
(Raytheon Co. United States)
Tuszynski, Andrew J.
(Columbus Technologies and Services, Inc. Pasadena, CA, United States)
Date Acquired
August 25, 2013
Publication Date
December 1, 2010
Publication Information
Publication: NASA Tech Briefs, December 2010
Subject Category
Engineering (General)
Report/Patent Number
NPO-45680
Distribution Limits
Public
Copyright
Public Use Permitted.
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