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Guidelines for structural verification and fracture control of Shuttle payloadsThe procedures followed by the NASA Office of the Chief Engineer in developing the guidelines concerning the structures, materials, and fracture control of the Space Shuttle payloads are described. Factors controlling the payload launch safety, such as crew and passenger safety, reusability, and mixes of payloads in a single launch are emphasized. Special consideration is given to the STS design and testing approaches, materials considerations, safety criticality review processes, nondestructive evaluation inspection for STS payload fracture control, fracture mechanics screening procedures, and components of special concern (e.g., pressurized vessels, fasteners, and composite structures).
Document ID
19860029644
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lifer, C. E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Lou, M. C.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Space Transportation
Report/Patent Number
AIAA PAPER 85-6082
Accession Number
86A14382
Distribution Limits
Public
Copyright
Other

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