Dynamic response of the LE-5 rocket engine liquid oxygen pump
Author:
Affiliation:
1. National Aerospace Laboratory of Japan, Miyagi, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.25731
Reference14 articles.
1. Longitudinal instability of liquid rockets due to propulsion feedback /POGO/.
2. Theoretical, quasi-static analysis of cavitation compliance in turbopumps.
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Japan's Liquid Propellant Rocket-Engine History;History of Liquid Propellant Rocket Engines;2006-01
2. Dynamic Response Analysis of High-Pressure Rocket Pumps;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2004
3. Geometry Effects in the Dynamic Response of Cavitating LE-7 Liquid Oxygen Pump;Journal of Propulsion and Power;1995-03
4. The effects of geometry in the dynamic response of the cavitating LE-7 LOX pump;29th Joint Propulsion Conference and Exhibit;1993-06-28
5. POGO analysis on the H-II launch vehicle;30th Structures, Structural Dynamics and Materials Conference;1989-04-03
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