This page no longer updated from 31 October 2001. Latest version can be found at RD-192.2

Manufacturer Name: RD-192.2. Designer: Glushko. Developed in: 1996-. Propellants: Lox/LCH4 Thrust(vac): 198,000 kgf. Thrust(vac): 1,942.00 kN. Isp: 354 sec. Isp (sea level): 325 sec. Diameter: 1.5 m. Length: 3.6 m. Chambers: 1. Chamber Pressure: 196.00 bar. Oxidizer to Fuel Ratio: 3.50. Country: Russia. Status: Developed 1996-on. References: 402 . Comments: Proposed variant of RD-192. Staged combustion cycle with fuel-rich gas generator. Gimbaling +/- 8 degree in two planes. Status 1998 was project based on RD-191 protoype, development estimated to take four years.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .