Effects of the Choice Between Kerosene and Methane on Size and Performance of Reusable Liquid Booster Stages
Author:
Affiliation:
1. DLR
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-5122
Reference22 articles.
1. Haeseler, D. et. al.: Testing of LOX-Hydrocarbon Thrust Chambers For Future Reusable Launch Vehicles,AIAA-2002-3845,July2002
2. Pempie, P. etal.: LOX/Methane and LOX/Kerosene High Thrust Engine Trade-off, AIAA-2001-3542, July2001
3. Accettura, A.G. etal.: Investigations and considerations about Reusable LOx/HC engines as key technologies for Future Launch Vehicles, AIAA-2002-3846, July2002
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