Encyclopedia Astronautica
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

15D23
KBMash solid rocket engine. RT-2 Stage 1. Out of Production. Three gimbaled nozzles for steering. Ammonium perchlorate/aluminum propellant. Chamber pressure 40 kgf/cm2.

Status: Out of Production. Date: 1961-1966. Thrust: 892.00 kN (200,529 lbf). Gross mass: 34,600 kg (76,200 lb). Unfuelled mass: 4,000 kg (8,800 lb). Burn time: 75 s. Height: 8.70 m (28.50 ft). Diameter: 1.84 m (6.03 ft).

Thrust (sl): 862.000 kN (193,785 lbf). Thrust (sl): 88,000 kgf.

Subtopics

15D23P TsKB-7 solid rocket engine. RT-2P Stage 1. Out of Production. Three gimbaled nozzles for steering. Ammonium perchlorate/ammonium butyl propellant. Chamber pressure 56 kgf/cm2.

Country: Russia. Launch Vehicles: RT-2. Propellants: Solid. Stages: 15D23. Agency: KBMash.

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
© 1997-2016 Mark Wade - Contact
© / Conditions for Use