|
15D94
|
|
Designer: TsKB-7. Developed in: 1968-1972. Application: RT-2P Stage 3. Gross Mass: 4,640 kg (10,220 lb). Empty Mass: 1,040 kg (2,290 lb). Propellants: Solid. Thrust(vac): 180.400 kN (40,556 lbf). Burn time: 49 sec. Diameter: 1.00 m (3.20 ft). Length: 5.45 m (17.88 ft). Chambers: 1. Country: Russia. Status: Out of Production. Three gimballed nozzles for steering. Ammonium perchlorate/ammonium butyl propellant. Chamber pressure 48 kgf/cm2.
|
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.
|
|
|
|