High-altitude simulation tests of the LOX/LH2 engine LE-5
Author:
Affiliation:
1. National Space Development Agency of Japan, Miyagi, Japan
2. National Aerospace Laboratory, Miyagi, Japan
3. Mitsubishi Heavy Industries Ltd., Nagoya, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.22779
Reference7 articles.
1. Button, G.P. and Ross, D.M., Rocket Propulsiton Elements, John Wiley & Sons, New York, 1976, pp.213-215.
2. Development of Liquid Oxygen and Hydrogen Turbopumps for the LE-5 Rocket Engine
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