Major Results of RD-120 Engine Thrust Increase Activities Conducted Within The Framework of "Sea Launch" Program

Details Major Results of RD-120 Engine Thrust Increase Activities Conducted Within The Framework of "Sea Launch" Program Major Results of RD-120 Engine Thrust Increase Activities Conducted Within The Framework of "Sea Launch" Program

Jan 2002

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2002iaf..confe.772f&link_type=abstract

IAF abstracts, 34th COSPAR Scientific Assembly, The Second World Space Congress, held 10-19 October, 2002 in Houston, TX, USA.,

Physics

Scientific paper

payload capabilities of "Zenit-3SL" launch vehicle that is intended to be launched from ocean-based platform in order to broaden the current segment of payload market. possible. thrust chamber cooling margins, stability of operation, and specific impulse. engine operation at increased thrust levels the safety factors of major assemblies, that are critical to the engine operation, meet the required safety standards. increased thrust levels has been made taking into account conducted hot fire tests. hot fire tests of the engine at increased thrust levels.

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