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Zenit-2M
Part of Zenit Family
Ukrainian orbital launch vehicle. Two-stage version of the Zenit-3SL booster developed for the Sea Launch program, modified for launch from ground facilities at Baikonur. Uses the common Zenit-2SB core vehicle with no upper stage.

AKA: Zenit-2SLB. Status: Active. First Launch: 2007-06-29. Last Launch: 2007-06-29. Number: 1 . Payload: 12,030 kg (26,520 lb). Thrust: 7,300.00 kN (1,641,100 lbf). Gross mass: 458,900 kg (1,011,700 lb). Height: 57.35 m (188.15 ft). Diameter: 3.90 m (12.70 ft). Apogee: 400 km (240 mi).

LEO Payload: 12,030 kg (26,520 lb) to a 400 km orbit at 51.60 degrees.


More at: Zenit-2M.

Family: orbital launch vehicle. Country: Ukraine. Spacecraft: Tselina-2. Launch Sites: Baikonur, Baikonur LC45/1. Stages: Zenit-A, Zenit-B. Agency: Yuzhnoye.

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