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Rokot K


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Rokot
Rokot launch vehicle Russian all-solid orbital launch vehicle. Version with Briz-K upper stage.

First Launch: 1994-12-26. Last Launch: 1999-12-24. Number: 2 . Payload: 1,850 kg (4,070 lb). Thrust: 1,870.00 kN (420,390 lbf). Gross mass: 107,000 kg (235,000 lb). Height: 29.00 m (95.00 ft). Diameter: 2.50 m (8.20 ft). Apogee: 1,500 km (900 mi).

LEO Payload: 1,850 kg (4,070 lb).

More at: Rokot K. Family: all-solid, orbital launch vehicle. Country: Russia. Stages: Rokot-3 Briz, UR-100N Stage 1N, UR-100N Stage 2N. Agency: Chelomei bureau. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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