DocumentCode
3515483
Title
Mars Science Laboratory - Backshell Interface Plate and Parachute Support Structure Subsystem
Author
Knight, Jennifer ; Ghan, Saina
Author_Institution
Jet Propulsion Lab., Pasadena, CA
fYear
2008
fDate
1-8 March 2008
Firstpage
1
Lastpage
6
Abstract
Mars Science Laboratory is a scientific mission to deliver a rover with ten science instruments to the surface of Mars. In order to accomplish this, a cruise stage and entry vehicle, which is comprised of an aeroshell and descent stage, are used. The backshell interface plate (BIP) interfaces to the backshell, the cruise stage and the descent stage. Also attached to the BIP is the parachute support structure (PSS) which interfaces to both structure and soft goods of the parachute deceleration system. The primary function of the BIP and PSS is to anchor all of these major subsystems together and provide the structural load paths necessary to support the launch, entry, mortar fire, and parachute inflation loads. The key challenges for this hardware lie in the complex configuration, several unique load cases, multiple load paths, and the magnitude of the loads. This paper will describe the design of the backshell interface plate and parachute support structure as well as the key challenges and how they were met.
Keywords
aerospace instrumentation; planetary rovers; space vehicles; Mars Science Laboratory; backshell interface plate; cruise stage; descent stage; parachute deceleration system; parachute support structure subsystem; rover; Assembly; Hardware; Instruments; Laboratories; Mars; Propulsion; Protection; Rough surfaces; Space vehicles; Surface roughness;
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.2008.4526540
Filename
4526540
Link To Document