Optimal pitch thrust-vector angle and benefits for all flight regimes
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Author
Contributions
- Bolonkin, Alexander. - Contributor
- NASA Dryden Flight Research Center. - Contributor
Publication
2000 - National Technical Information Service, distributor, Edwards, Calif, California
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- OCLC Control Number45009655
- Open LibraryOL18318816M
Alternate Titles
- Optimal pitch thrust vector angle and benefits for all flight regimes
Subjects
Series Statement
- [NASA technical memorandum] -- NASA/TM-2000-209021
- NASA technical memorandum -- 209021.
Other Editions
- Optimal pitch thrust-vector angle and benefits for all flight regimes
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