DocumentCode :
3206504
Title :
Tension-only, moment-free, separation mechanism for Mars Science Laboratory aeroshell
Author :
Buecher, David ; Hund, Richard
Author_Institution :
Lockheed Martin Space Syst. Co., Littleton, CO
fYear :
2009
fDate :
7-14 March 2009
Firstpage :
1
Lastpage :
9
Abstract :
Lockheed Martin Space Systems Company is involved in the design and manufacture of the aeroshell for the Mars Science Laboratory (MSL) rover, an upcoming NASA-JPL mission to Mars. During entry into the Martian atmosphere, the aeroshell primarily protects the rover, as the spacecraft passes through extreme heating and dynamic pressure environments. After entering the atmosphere, and decelerating, the nine separation mechanisms, located at the Backshell to Heatshield interface, separate the aeroshell at the seam between the Heatshield (the lee-side, or entry half, of the aeroshell) and the Backshell (the aft-side of the aeroshell), to enable the successful deployment of the lander.
Keywords :
aerospace engineering; aerospace industry; bending; compressive strength; design engineering; planetary rovers; Heatshield entry loads; Heatshield separation hardware; Lockheed Martin Space Systems Company; Mars Science Laboratory Aeroshell; Mars Science Laboratory rover; Martian atmosphere; NASA-JPL mission; backshell ring; bending loads; compressive force; compressive loads; moment-free separation mechanism; parachute inflation; separation fittings; shear loads; tension loads; tension-only separation mechanism; Aerodynamics; Atmosphere; Fitting; Laboratories; Manufacturing; Mars; Performance evaluation; Protection; Testing; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace conference, 2009 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4244-2621-8
Electronic_ISBN :
978-1-4244-2622-5
Type :
conf
DOI :
10.1109/AERO.2009.4839585
Filename :
4839585
Link To Document :
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