Cryogenic Spray Ignition at High Altitude Conditions

Author:

De Rosa Marco,Sender Jo,Zimmermann Herbert,Oschwald Michael

Publisher

American Institute of Aeronautics and Astronautics

Reference9 articles.

1. Ignition of cryogenic H2/LOX sprays

2. 2Schmidt, V., Klimenko, D., Haidn, O., Oschwald, M., Nicole, A., Ordonneau, G., Habiballah, M. "Experimental Investigation and Modelling of the Ignition Transient of a Coaxial H2/O2-Injector", 5th International Symposium on Liquid SpacePropulsion, Chattanooga,TN, USA, October 2003.

3. 3Schmidt, V., Wepler, U., Haidn, O.J., Oschwald, M. "Characterization of the Primary Ignition Process of a Coaxial GH2/LOX Spray", AIAA 2004-1167,42ndAerospace Science Meeting, Reno, NV, USA,January2004.

4. 5Krühsel,G.;Schäfer,K.;Kronmüller,H.;Zimmermann,H."P4.1TestfacilityforhighaltitudesimulationofVinciengine-BenchDevelopment",1stEuropean Conference forAerospace Sciences EUCASS, July2-4,2005,Moscow,Russia

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