Cryogenic liquid rocket engine technology developments within the German National Technology Programme
Author:
Affiliation:
1. Daimler-Benz Aerospace AG, Munich, Germany
2. DLR, Hauptabt. Raumfahrtantriebe, Hardthausen, Germany
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2822
Reference20 articles.
1. FESTIP system study - An overview
2. Numerical simulation of transients in feed systems for cryogenic rocket engines
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