|
RD-0244-HC
|
|
Manufacturer Name: RD-0244-HC. Other Designations: RD-0244 KD. Designer: Kosberg. Propellants: Lox/Kerosene. Thrust(vac): 690.000 kN (155,110 lbf). Isp: 332 sec. Mass Engine: 540 kg (1,190 lb). Chambers: 1. Chamber Pressure: 230.00 bar. Oxidizer to Fuel Ratio: 2.70. Thrust to Weight Ratio: 130.29. Country: Russia. Status: Design concept 1990's. Proposed variant of RD-0244 engine using LOX-kerosene instead of N2O4/UDMH as propellants.
Bibliography and Further Reading - Russian Arms Catalogue, Vol 5 and 6, Military Parade, Moscow via Dietrich Haeseler.
|
Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.
© Mark Wade, 1997 - 2007 except where otherwise noted.
|
|
|
|