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Human Rating the Orion Parachute SystemHuman rating begins with design. Converging on the requirements and identifying the risks as early as possible in the design process is essential. Understanding of the interaction between the recovery system and the spacecraft will in large part dictate the achievable reliability of the final design. Component and complete system full-scale flight testing is critical to assure a realistic evaluation of the performance and reliability of the parachute system. However, because testing is so often difficult and expensive, comprehensive analysis of test results and correlation to accurate modeling completes the human rating process. The National Aeronautics and Space Administration (NASA) Orion program uses parachutes to stabilize and decelerate the Crew Exploration Vehicle (CEV) spacecraft during subsonic flight in order to deliver a safe water landing. This paper describes the approach that CEV Parachute Assembly System (CPAS) will take to human rate the parachute recovery system for the CEV.
Document ID
20110011095
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Machin, Ricardo A.
(NASA Johnson Space Center Houston, TX, United States)
Fisher, Timothy E.
(NASA Johnson Space Center Houston, TX, United States)
Evans, Carol T.
(NASA Johnson Space Center Houston, TX, United States)
Stewart, Christine E.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2011
Subject Category
Space Transportation And Safety
Report/Patent Number
JSC-CN-22974
Meeting Information
Meeting: 21st AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar
Location: Dublin
Country: Ireland
Start Date: May 23, 2011
End Date: May 26, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 644423.06.31.04.03.10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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