Preliminary Design of the Cruise, Entry, Descent, and Landing Mechanical Subsystem for MSL-Reference-Cited by-同舟云学术

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Preliminary Design of the Cruise, Entry, Descent, and Landing Mechanical Subsystem for MSL

Published:2007 Issue: Volume: Page:
ISSN:
Container-title:2007 IEEE Aerospace Conference
language:
Short-container-title:

Author:

Hoffman Pamela,Rivillini Tomasso,Slimko Eric,Dahya Neilesh,Agajanian Anthony,Knight Jennifer,Sengupta Anita,Thoma Benjamin,Webster Richard,Gallon John,Gradziel Michael

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx5/4161231/4144550/04161342.pdf?arnumber=4161342

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3. Supersonic Testing of 0.8 m Disk Gap Band Parachutes in the Wake of a 70 deg Sphere Cone Entry Vehicle;20th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar;2009-05-04

4. Findings from the Supersonic Qualification Program of the Mars Science Laboratory Parachute System;20th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar;2009-05-04

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