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Secondary structures and mechanisms - Design trouble area for the space shuttleThe design of secondary structures and mechanisms for a reusable space shuttle can produce problems as serious as those involved in designing the primary structure and thermal protection system. Several events involving failure of secondary structures during the X-15 flight program have been selected to illustrate potential problem areas. Similar problems may be expected on future reusable vehicles until additional research provides adequate design information in these areas.
Document ID
19700033667
Acquisition Source
Ames Research Center
Document Type
Contribution to a larger work
Authors
Eldon E. Kordes
(Armstrong Flight Research Center Edwards, United States)
Date Acquired
August 5, 2013
Publication Date
July 1, 1970
Publication Information
Publication: Space Transportation System Technology Symposium III - Structures and Materials
Publisher: National Aeronautics and Space Administration
Volume: NASA-TM-X-52876-VOL-III
Issue Publication Date: June 30, 1970
Subject Category
Space Vehicles
Meeting Information
Meeting: Space Transportation System Technology Symposium
Location: Cleveland, OH
Country: US
Start Date: July 15, 1970
End Date: July 17, 1970
Sponsors: Glenn Research Center
Accession Number
70N42983
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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