DocumentCode
3515360
Title
Guide Rails for Linear Separation of Powered Descent Vehicle from Mars Science Laboratory Backshell
Author
Quicksall, J.J. ; Gallon, J.C.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
fYear
2008
fDate
1-8 March 2008
Firstpage
1
Lastpage
6
Abstract
During descent through the Martian atmosphere, Mars science laboratory (MSL) uses three sets of guide rails and rollers to control the separation dynamics of the powered descent vehicle (PDV) from the Backshell and parachute. The guided linear separation of the two bodies over a distance of half a meter mitigates the risk of re- contact which could result in unexpected and detrimental vehicle dynamics. The guide rails are comprised of three thin beams oriented in 120 degree intervals around the circumference of the Backshell´s internal structure, and they interface with three sets of four rollers mounted on the exterior of the PDV. This configuration resists motion in 5 DOF. The only unconstrained DOF is in the direction of desired separation. Analysis was used to size the guide rail and rollers, and tests will be performed to validate the design´s capability to perform as required during the dynamic separation event.
Keywords
aerospace components; rails; space vehicles; Mars science laboratory backshell; Martian atmosphere; guide rails; linear separation; parachute; powered descent vehicle; rollers; vehicle dynamics; Atmosphere; Laboratories; Mars; Performance evaluation; Rails; Resists; Space vehicles; Vehicle driving; Vehicle dynamics; Wrist;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2008 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-1487-1
Electronic_ISBN
1095-323X
Type
conf
DOI
10.1109/AERO.2008.4526534
Filename
4526534
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