Design and operational aspect of LOX/LH2 propulsion system of reusable vehicle testing (RVT)
Author:
Affiliation:
1. Inst. of Space and Astronautical Science, Sagamihara, Japan
2. Ishikawajima-Harima Heavy Industries Co., Ltd., Mizuho, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-1841
Reference5 articles.
1. Concept and Preliminary Flight Testing of a Fully Reusable Rocket Vehicle
2. Yamakawa, H., Higuchi, K., Maruyama, T, and Kubota, N. "Flight Evaluation of GN&C System and Vertical Landing Dynamics of Reusable Rocket Vehicle,"AIAAPaper 2001-1907,April 2001.
3. Brewer,G. D., Hydrogen Aircraft Technology, 1st ed.CRCPress,BocaRaton,FL,1991, pp.138-158.
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