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Molniya 8K78M SOL
Part of R-7 Family
Russian orbital launch vehicle. Improved Molniya variant with Blok SO-L upper stage for placement of Prognoz-class satellites in orbits with apogees of 200,000 km.

First Launch: 1972-04-14. Last Launch: 1985-04-26. Number: 10 . 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: 400,000 km (240,000 mi).

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


More at: Molniya 8K78M SOL.

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

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