Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
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Author
Contributions
- Engelund, W. C. - Contributor
- United States. National Aeronautics and Space Administration. - Contributor
Publication
1997 - National Aeronautics and Space Administration, [Washington, DC, District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- OCLC Control Number38290177
- Open LibraryOL17121322M
Alternate Titles
- Subsonic to hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
Subjects
Series Statement
- NASA TM -- 111926
- AIAA -- 95-1848
- NASA technical memorandum -- 111926..
Other Editions
- Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
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