Propellant atomization in LOX/GH2 rocket engines
Author:
Affiliation:
1. DLR, Hardthausen, Germany
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3685
Reference11 articles.
1. Cryogenic liquid rocket engine technology developments within the German National Technology Programme
2. Coaxial atomization of a round liquid jet in a high speed gas stream: A phenomenological study
3. Propellant injection in a liquid oxygen/gaseous hydrogen rocket engine
4. Injection and mixing processes in high pressure LOX/GH2 rocket combustors
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