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Integrated Airframe DemonstrationsThe objective of the project described in this viewgraph presentation is to develop and verify the technology required for the application of minimal weight control surfaces that meet MASP vehicle requirements. The approaches include the development of design and fabrication concepts, the verification of concept design through sub-component fabrication and tests, the design and fabrication of a full-scale segment of the carbon-carbon control surface, and the design verification and fabrication technology by thermal and structural tests.
Document ID
20010082359
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Glass, David E.
(NASA Langley Research Center Hampton, VA United States)
Sawyer, J. Wayne
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 20, 2013
Publication Date
October 3, 2000
Publication Information
Publication: ST Day 2000: Risk Reduction for The Next Generations
Subject Category
Space Transportation And Safety
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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