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An Approach to Risk-Based Design Incorporating Damage Tolerance AnalysesIncorporating risk-based design as an integral part of spacecraft development is becoming more and more common. Assessment of uncertainties associated with design parameters and environmental aspects such as loading provides increased knowledge of the design and its performance. Results of such studies can contribute to mitigating risk through a system-level assessment. Understanding the risk of an event occurring, the probability of its occurrence, and the consequences of its occurrence can lead to robust, reliable designs. This paper describes an approach to risk-based structural design incorporating damage-tolerance analysis. The application of this approach to a candidate Earth-entry vehicle is described. The emphasis of the paper is on describing an approach for establishing damage-tolerant structural response inputs to a system-level probabilistic risk assessment.
Document ID
20020039140
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Knight, Norman F., Jr.
(Veridian Systems Div. Chantilly, VA United States)
Glaessgen, Edward H.
(NASA Langley Research Center Hampton, VA United States)
Sleight, David W.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Quality Assurance And Reliability
Report/Patent Number
AIAA Paper 2002-1267
Report Number: AIAA Paper 2002-1267
Meeting Information
Meeting: 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Denver, CO
Country: United States
Start Date: April 22, 2002
End Date: April 25, 2002
Sponsors: American Helicopter Society, Inc., American Society for Composites, American Society of Mechanical Engineers, American Society of Mechanical Engineers, American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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