Molniya 8K78/E6

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Molniya 8K78/E6

Part of R-7

Russian orbital launch vehicle. Molniya adaptation for launch of E-6 lunar probes.

Status: Retired 1965. Thrust: 4,054.00 kN (911,375 lbf). Gross mass: 306,200 kg (675,000 lb). Height: 44.40 m (145.60 ft). Diameter: 2.95 m (9.67 ft). Apogee: 400,000 km (240,000 mi).

Family: orbital launch vehicle. Country: Russia. Spacecraft: Luna E-6. Projects: Luna. Launch Sites: Baikonur, Baikonur LC1. Stages: Molniya 8K78-0, Molniya 8K78-1, Molniya 8K78-2, Molniya 8K78-3. Agency: Korolev bureau.

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