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
15D25
Status: Out of Production. Date: 1961-1966. Thrust: 137.00 kN (30,798 lbf). Gross mass: 3,500 kg (7,700 lb). Unfuelled mass: 1,000 kg (2,200 lb). Burn time: 45 s. Height: 3.83 m (12.56 ft). Diameter: 0.98 m (3.21 ft).
| 15D94 TsKB-7 solid rocket engine. RT-2P Stage 3. Out of Production. Three gimbaled nozzles for steering. Ammonium perchlorate/ammonium butyl propellant. Chamber pressure 48 kgf/cm2. |
Country: Russia. Launch Vehicles: RT-2. Propellants: Solid. Stages: 15D25. Agency: KBMash.
Back to top of page
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use