Hypersonic airframe structures technology needs and flight test requirements/
Main Author: | Stone, J. E. |
---|---|
Corporate Authors: | United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center, McDonnell Douglas Corporation |
Other Authors: | Koch, L. C. |
Format: | Book |
Language: | English |
Published: |
Washington, D.C.:
National Aeronautics and Space Administration, Scientific and Technical Information Branch,
1979
|
Series: | NASA contractor report
3130 |
Subjects: |
Similar Items
-
Hypersonic technology for military application
Published: (1989) -
Loading tests of a wing structure for a hypersonic aircraft/
by: Fields, Roger A.
Published: (1980) -
High heat flux actively cooled honeycomb sandwich structural panel for a hypersonic aircraft/
by: Koch, L. C.
Published: (1978) -
Scramjet nozzle design and analysis as applied to a highly integrated hypersonic research airplane/
by: Small, William J. 1939-
Published: (1976) -
Development and validation of purged thermal protection systems for liquid hydrogen fuel tanks of hypersonic vehicles/
by: Helenbrook, R. G.
Published: (1977)