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Application of the QSDC procedure to the formulation of space shuttle design criteria. Volume 2: Applications guideCriteria to determine the probability of aircraft structural failure were established according to the Quantitative Structural Design Criteria by Statistical Methods, the QSDC Procedure. This criteria method was applied to the design of the space shuttle during this contract. An Applications Guide was developed to demonstrate the utilization of the QSDC Procedure, with examples of the application to a hypothetical space shuttle illustrating the application to specific design problems. Discussions of the basic parameters of the QSDC Procedure: the Limit and Omega Conditions, and the strength scatter, have been included. Available data pertinent to the estimation of the strength scatter have also been included.
Document ID
19720023207
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bouton, I.
(Technology, Inc. Dayton, OH, United States)
Martin, G. L.
(Technology, Inc. Dayton, OH, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1972
Subject Category
Space Vehicles
Report/Patent Number
TI-425-72-14-VOL-2
NASA-CR-123786
Report Number: TI-425-72-14-VOL-2
Report Number: NASA-CR-123786
Accession Number
72N30857
Funding Number(s)
CONTRACT_GRANT: NAS8-26918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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