Testing of LOX-Hydrocarbon Thrust Chambers For Future Reusable Launch Vehicles-Reference-Cited by-同舟云学术

Testing of LOX-Hydrocarbon Thrust Chambers For Future Reusable Launch Vehicles

Published:2002-07-07 Issue: Volume: Page:
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Container-title:38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Haeseler Dietrich,Goetz Andreas,Mäding Chris,Roubinski Vitali,Khrissanfov Sergey,Berejnoy Viktor

Publisher

American Institute of Aeronautics and Astronautics

Reference11 articles.

1. D. Haeseler, A. Gotz, C. Mading. V. Roubinski, V. Gorokhov, S. Khrissanfov: Combustion Chambers and Engine Concepts UsingHydrocarbon Fuelsfor Futun Launch I.khjJ.s, IAF-01-5.3.06, 52nd International Astronautical Congress, October 200I, Toulouse,France.

2. D. Haeseler, A. Gotz, A. Frohlich: Non-Toxic Propellants for Future Advanced Launcher Propulsion Systems, AIAA-2000-3687, 36thAIAA Joint Propulsion Conference, July 2000, Huntsville, AL.

3. J.E. Quinn: Cost Trade-offfor a Pressure-fedLiquid Rocket to LEO, AIAA 99-2622, 35th AIAA Joint Propulsion Conference, June 1999, Los Angeles, USA.

4. L. Schoenmann: LOMPropane and LOMEthanol Combustion Chamber Heat Transfer,J. PropulsionVol.7NO. 4 pp.538-548 (AIAA-87-1857)

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