A study on versatile simulation of liquid propellant rocket engine systems transients-Reference-Cited by-同舟云学术

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A study on versatile simulation of liquid propellant rocket engine systems transients

Published:2000-07-24 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Liu Kun¹,Zhang Yulin¹

Affiliation:

1. National Univ. of Defense Technology, Changsha, China

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3771

Reference17 articles.

1. SSME model, engine dynamic characteristics related to POGO.N76-15264,1973

2. Akio KANMURI, etal Start Transient Analysis of Turbopump-fed LOX/LH2 Rocket Engine(LE-5). N86-19371,1983

3. E. K. Ruth, H. Ahn, R. L. Baker, and M. A. Brosmer. Advanced Liquid RocketEngine TransientModel AlAA 90-2299

4. F.Y Kuo. Space Shuttle Main Engine Real-timeStability Analysis.AIAA 93-2078

5. M. P. Binder. A Transient Model of the RL10A-3-3A Rocket Engine NASA CR-195478(AIAA 95-2968)

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