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Molniya 8K78M ML
Part of R-7
Russian orbital launch vehicle. Improved Molniya variant with Blok-ML upper stage for placement of communications satellites into Molniya-class orbits with apogees of 38,500 km.

First Launch: 1970-08-17. Last Launch: 1972-03-31. Number: 4 . Payload: 2,000 kg (4,400 lb). Thrust: 4,054.00 kN (911,375 lbf). Gross mass: 305,000 kg (672,000 lb). Height: 43.40 m (142.30 ft). Diameter: 2.95 m (9.67 ft). Apogee: 40,000 km (24,000 mi).

Payload: 2,000 kg (4,400 lb) to a GTO.


More at: Molniya 8K78M ML.

Family: orbital launch vehicle. Country: Russia. Stages: Soyuz 11A511U2-2, Molniya 8K78M-0, Molniya 8K78M-1, Molniya M-3. Agency: Korolev bureau.

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