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
Link To Document :
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