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RD RT-15-2


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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 RD RT-15-2 Part of 15D24 OKB-1 solid rocket engine. RT-1 second stage.

AKA: RT-1-2. Status: Retired 1965. Thrust: 500.00 kN (112,400 lbf). Gross mass: 10,000 kg (22,000 lb). Unfuelled mass: 1,500 kg (3,300 lb). Burn time: 30 s. Height: 4.00 m (13.10 ft). Diameter: 1.49 m (4.88 ft).

Country: Russia. Launch Vehicles: RT-1. Propellants: Solid. Stages: RD RT-15-2. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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