DocumentCode
3206562
Title
MSL V&V CEDL Mechanical Systems test program
Author
Eremenko, Alexander ; Hoffman, Pamela ; Rivellini, Tommaso
Author_Institution
Jet Propulsion Lab., NASA, Pasadena, CA
fYear
2009
fDate
7-14 March 2009
Firstpage
1
Lastpage
9
Abstract
Mars Science Laboratory is a scientific mission with exploration rover. In order to accomplish this mission, the rover must be transported from Earth to the Martian surface, including cruise, entry, descent, and landing phases (CEDL). The key challenges for testing CEDL mechanical system lie in the physical size of the spacecraft and major subassemblies, complex configuration, multiple load cases, numerous separation events, new unique ldquosky cranerdquo landing method, budget and schedule limitations, and difficulties associated with testing in Earth environments. This paper will describe the verification and validation (V&V) CEDL mechanical systems test program and key challenges of each of subsystem testsrdquo.
Keywords
Mars; aerospace engineering; aerospace testing; mechanical testing; space vehicles; Martian surface; mechanical systems test program; rover; scientific mission; spacecraft; Cranes; Earth; Laboratories; Mechanical systems; NASA; Propulsion; Safety; Space vehicles; System testing; Vibrations;
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.2009.4839588
Filename
4839588
Link To Document