|
RD-182M
|
|
Manufacturer Name: RD-182M. Designer: Glushko. Developed in: 1998-. Application: Vozdushnyy Start stage 1. Propellants: Lox/LNG. Thrust(vac): 882.000 kN (198,281 lbf). Chambers: 1. Country: Russia. Status: Developed 1998-. Variant of RD-182 engine for liquid natural gas (mainly CH4). Proposed initial candidate for project Vozdushnyy Start of Kompomash.
Bibliography and Further Reading - Polovnikov S P; Karpov, A S, Vestnik Aviatsii i Kosmonavtiki, "Projekt 'Vozdushnyy Start'", Moscow, 1-2/98 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.
|
|
|
|