15D24P

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z

15D24P

Part of 15D24

TsKB-7 solid rocket engine. RT-2P Stage 2. Out of Production. Three gimbaled nozzles for steering. Ammonium perchlorate/ammonium butyl propellant. Chamber pressure 48 kgf/cm2.

Status: Out of Production. Date: 1968-1972. Thrust: 437.30 kN (98,309 lbf). Gross mass: 11,280 kg (24,860 lb). Unfuelled mass: 1,500 kg (3,300 lb). Burn time: 61 s. Height: 5.08 m (16.66 ft). Diameter: 1.49 m (4.88 ft).

Country: Russia. Launch Vehicles: RT-2P. Propellants: Solid. Agency: TsKB-7.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z