|
RD-0124-14D23
|
|
Manufacturer Name: RD-0124-14D23. Government Designation: 14D23. Designer: Kosberg. Application: Angara stage 2 verniers. Kvant-1 stage 1 vernier. Propellants: Lox/Kerosene. Thrust(vac): 298.640 kN (67,137 lbf). Isp: 331 sec. Burn time: 300 sec. Chambers: 4. Chamber Pressure: 173.50 bar. Oxidizer to Fuel Ratio: 2.60. Country: Russia. Status: Designed 1986-1990. Variant of RD-0124 with shortened nozzle for sea-level operation. Proposed for small launcher Kvant-1 by RKK Energia for stage 1 steering engine. Also proposed by RKK Energia in initial studies in 1993 for Angara upper stage.
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.
|
|
|
|