DocumentCode
1885871
Title
Verification and validation testing of the Bridle and Umbilical Device for Mars Science Laboratory
Author
Gallon, John
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear
2012
fDate
3-10 March 2012
Firstpage
1
Lastpage
16
Abstract
The Bridle Umbilical Device (BUD) subsystem is used during the Skycrane maneuver of the Mars Science Laboratory (MSL) during the final phases of the Entry Descent and Landing (EDL). During this phase the BUD subsystem will control the deployment of the MSL Rover from the Descent Stage. This paper covers the verification and validation testing of the subsystem. Testing included component through full system level testing. Testing ranged from simple bench top extraction tests to full system deploy drop test that included external disturbances such as the Rover mobility impulse. This paper will discuss the test that were performed, why they were performed and how these test results were used in the overall Verification and Validation of the MSL Skycrane phase.
Keywords
Mars; planetary rovers; BUD subsystem; EDL; MSL Rover; MSL Skycrane phase; Mars science laboratory; Rover mobility impulse; bridle umbilical device subsystem; full system level testing; Assembly; Laboratories; Mars; Pulleys; Springs; Torque;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2012 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4577-0556-4
Type
conf
DOI
10.1109/AERO.2012.6187289
Filename
6187289
Link To Document