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Best Practices for Reliable and Robust Spacecraft StructuresA study was undertaken to capture the best practices for the development of reliable and robust spacecraft structures for NASA s next generation cargo and crewed launch vehicles. In this study, the NASA heritage programs such as Mercury, Gemini, Apollo, and the Space Shuttle program were examined. A series of lessons learned during the NASA and DoD heritage programs are captured. The processes that "make the right structural system" are examined along with the processes to "make the structural system right". The impact of technology advancements in materials and analysis and testing methods on reliability and robustness of spacecraft structures is studied. The best practices and lessons learned are extracted from these studies. Since the first human space flight, the best practices for reliable and robust spacecraft structures appear to be well established, understood, and articulated by each generation of designers and engineers. However, these best practices apparently have not always been followed. When the best practices are ignored or short cuts are taken, risks accumulate, and reliability suffers. Thus program managers need to be vigilant of circumstances and situations that tend to violate best practices. Adherence to the best practices may help develop spacecraft systems with high reliability and robustness against certain anomalies and unforeseen events.
Document ID
20070021484
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Raju, Ivatury S.
(NASA Langley Research Center Hampton, VA, United States)
Murthy, P. L. N.
(NASA Glenn Research Center Cleveland, OH, United States)
Patel, Naresh R.
(Aerospace Corp. El Segundo, CA, United States)
Bonacuse, Peter J.
(Army Research Lab. Hampton, VA, United States)
Elliott, Kenny B.
(NASA Langley Research Center Hampton, VA, United States)
Gordon, S. A.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Gyekenyesi, J. P.
(NASA Glenn Research Center Cleveland, OH, United States)
Daso, E. O.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Aggarwal, P.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Tillman, R. F.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2007
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA 2007-2270
Report Number: AIAA 2007-2270
Meeting Information
Meeting: 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Location: Waikiki, HI
Country: United States
Start Date: April 23, 2007
End Date: April 26, 2007
Sponsors: American Society for Composites, American Helicopter Society, Inc., American Society of Mechanical Engineers, American Society of Civil Engineers, American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 510505.03.07.01.11
Distribution Limits
Public
Copyright
Public Use Permitted.
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