A model for the space shuttle main engine high pressure oxidizer turbopump shaft seal system
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Author
Contributions
- United States. National Aeronautics and Space Administration. - Contributor
Publication
1991 - For sale by the National Technical Information Service, Washington, DC, District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- Open LibraryOL15294683M
Subjects
Topics
Series Statement
- NASA technical memorandum -- 103697.
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