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Verification and Validation of Requirements on the CEV Parachute Assembly System Using Design of ExperimentsThe Crew Exploration Vehicle Parachute Assembly System (CPAS) project conducts computer simulations to verify that flight performance requirements on parachute loads and terminal rate of descent are met. Design of Experiments (DoE) provides a systematic method for variation of simulation input parameters. When implemented and interpreted correctly, a DoE study of parachute simulation tools indicates values and combinations of parameters that may cause requirement limits to be violated. This paper describes one implementation of DoE that is currently being developed by CPAS, explains how DoE results can be interpreted, and presents the results of several preliminary studies. The potential uses of DoE to validate parachute simulation models and verify requirements are also explored.
Document ID
20110011157
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Schulte, Peter Z.
(Jacobs Technologies Engineering Science Contract Group Houston, TX, United States)
Moore, James W.
(Jacobs Technologies Engineering Science Contract Group Houston, TX, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2011
Subject Category
Astronautics (General)
Report/Patent Number
JSC-CN-23423
Report Number: JSC-CN-23423
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
Public Use Permitted.
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