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Approximation Model Building for Reliability & Maintainability Characteristics of Reusable Launch VehiclesThis paper describes the development of parametric models for estimating operational reliability and maintainability (R&M) characteristics for reusable vehicle concepts, based on vehicle size and technology support level. A R&M analysis tool (RMAT) and response surface methods are utilized to build parametric approximation models for rapidly estimating operational R&M characteristics such as mission completion reliability. These models that approximate RMAT, can then be utilized for fast analysis of operational requirements, for lifecycle cost estimating and for multidisciplinary sign optimization.
Document ID
20000115873
Acquisition Source
Langley Research Center
Document Type
Reprint (Version printed in journal)
Authors
Unal, Resit
(Old Dominion Univ. Norfolk, VA United States)
Morris, W. Douglas
(NASA Langley Research Center Hampton, VA United States)
White, Nancy H.
(NASA Langley Research Center Hampton, VA United States)
Lepsch, Roger A.
(NASA Langley Research Center Hampton, VA United States)
Brown, Richard W.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
AIAA Paper 2000-4712
Report Number: AIAA Paper 2000-4712
Meeting Information
Meeting: Aviation, Range and Aerospace Meteorology
Location: Orlando, FL
Country: United States
Start Date: September 11, 2000
End Date: September 15, 2000
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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