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Defining Support Requirements During Conceptual Design of Reusable Launch VehiclesCurrent methods for defining the operational support requirements of new systems are data intensive and require significant design information. Methods are being developed to aid in the analysis process of defining support requirements for new launch vehicles during their conceptual design phase that work with the level of information available during this phase. These methods will provide support assessments based on the vehicle design and the operating scenarios. The results can be used both to define expected support requirements for new launch vehicle designs and to help evaluate the benefits of using new technologies. This paper describes the models, their current status, and provides examples of their use.
Document ID
20040111234
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Morris, W. D.
(NASA Langley Research Center Hampton, VA, United States)
White, N. H.
(NASA Langley Research Center Hampton, VA, United States)
Davis, W. T.
(NASA Langley Research Center Hampton, VA, United States)
Ebeling, C. E.
(Dayton Univ. OH, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1995
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 95-3619
Meeting Information
Meeting: AIAA 1995 Space Programs and Technologies Conference
Location: Huntsville, AL
Country: United States
Start Date: September 26, 1995
End Date: September 28, 1995
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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