|
RD-134R
|
|
Manufacturer Name: RD-134R. Government Designation: 11D123. Other Designations: RD-123. Designer: Glushko. Developed in: 1993. Application: Angara stage 2 vernier. Propellants: Lox/Kerosene. Thrust(vac): 343.000 kN (77,109 lbf). Chambers: 4 (?). Country: Russia. Status: Design concept 1993-on. Proposed in initial study for Angara by RKK Energia in1993. Steering engines for Angara upper stage. Kerosene RG-1.
Bibliography and Further Reading - Semenov, Yuri P Editor, Raketno-kosmicheskaya korporatsiya 'Energia' imeni S P Koroleva, Moscow, Russia, 1996. Russian in-house history of the Energia Corporation and its predecessors. Unprecedented detail, photographs, designations, and drawings, on the products of Korolev's OKB.
|
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.
|
|
|
|