Investigations and Considerations about Reusable LOX-HC Engines as Key Technology for Future Launch Vehicles-Reference-Cited by-同舟云学术

Investigations and Considerations about Reusable LOX-HC Engines as Key Technology for Future 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:

Accettura Antonio,De Rose Leonardo,Ierardo Nicola,Mascanzoni Flavia,Cuoco Francesco

Publisher

American Institute of Aeronautics and Astronautics

Reference7 articles.

1. Ierardo, N. Accettura, A. "LOX-HC:Current status and modelling of supercritical injectors", IAF-01-S.3.07,IAF Congress, October 2001, Toulouse,France.

2. Congiunti, A., Bruno, c. et al, "Cooling potential of High Pressure CH4", ISTS 2002-a-29, 23rdInternationalSymposiumonSpaceTechnologyand Science,Matsue,Japan.

3. Borromee, J., Eury, S. "Future European Reusable Propulsion Systems", AAAF,6th International Symposium on Propulsion for Space Transportation of the XXIst Century, Versaille, France.

4. Ierardo, N., Mascanzoni, F., Accettura, A.G. "Advanced LRE Technologies in the Frame of the Italian National Program FAST2", 16-118-P,6th International Symposium on Propulsion for Space Transportation of the XXIst Century, 14-17May 2002, Versailles, France.

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