Molniya 8K78M ML

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z

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.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z