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Effect of chamber pressure, flow per element, and contraction ratio on acoustic-mode instability in hydrogen-oxygen rockets / by John P. Wanhainen, Charles E. Feiler, and C. Joe Morgan.
Connect to full text Available online
View online- Format:
- Book
- Government document
- Author/Creator:
- Wanhainen, John P., author.
- Feiler, Charles E., author.
- Morgan, C. Joe, author.
- Series:
- NASA technical note ; D-4733.
- NASA technical note ; TN D-4733
- Language:
- English
- Subjects (All):
- Rocket engines--Thrust--Testing.
- Rocket engines.
- Stability of rockets.
- Physical Description:
- 1 online resource (ii, 35 pages) : illustrations.
- Place of Publication:
- Washington, D.C. : National Aeronautics and Space Administration, August 1968.
- Notes:
- "August 1968."
- Includes bibliographical references (page 35).
- Description based on online resource, PDF version; title from title page (NASA, viewed on Dec. 8, 2020).
- Electronic reproduction. [Place of publication not identified]: HathiTrust Digital Library. 2024.
- Other Format:
- Print version: Wanhainen, John P. Effect of chamber pressure, flow per element, and contraction ratio on acoustic-mode instability in hydrogen-oxygen rockets.
- OCLC:
- 761129117
- Access Restriction:
- Use copy Restrictions unspecified
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