This page no longer updated from 31 October 2001. Latest version can be found at RD-0124M1

Manufacturer Name: RD-0124M1. Designer: Kosberg. Developed in: 1998-. Propellants: Lox/Kerosene Thrust(vac): 30,000 kgf. Thrust(vac): 294.30 kN. Isp: 359 sec. Burn time: 300 sec. Mass Engine: 393 kg. Diameter: 1.5 m. Length: 2.6 m. Chambers: 1. Chamber Pressure: 157.00 bar. Country: Russia. Status: Developed 1998-. References: 312 . Comments: Proposed single chamber variant of RD-0124. Obviously same turbopumps, but one single chamber with larger nozzle extension compared to RD-0124M.
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 .