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Development of carbon-carbon nozzle extension for liquid fuel rocket motors
Authors:M. I. Sokolovsky  S. N. Petukhov  Yu. P. Semyonov  B. A. Sokolov
Affiliation:(1) SPA “Iskra”, Perm, Russia;(2) Korolev RSC “Energy”, Moscow, Russia
Abstract:
Successful experience of RSC “Energy” and SPA “Iskra” in the development of carbon-carbon extension for oxygen-kerosene liquid fuel rocket motor has been summarized. Methodological approach that served to completion of carbon-carbon extension development in full and at comparatively small expenses has been described. Results of practical application of carbon-carbon extension for liquid fuel rocket motor 11D58M have been presented within the framework of International Space Program “Sea Launch”.
Keywords:liquid fuel rocket motor (LFRM)  carbon-carbon extension
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