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Molniya 8K78M-PVB

R-7 familyProgress Rocket Space CenterRetired

A Russian orbital launch vehicle. Version of Molniya 8k78M with safety modifications to prevent and resist fires in all stages and the avionics compartment.

Molniya 8K78M-PVB vehicle

Specifications

Thrust
4,016 kN
Height
43.4 m
Diameter
2.95 m
Launch mass
305 t
Stages
3
LEO capacity
1,800 kg

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

8flightswith a definitive outcome
100%success rate8 of 8
0failuresincluding partial failures
8success streakcurrent

First flight July 25, 1990 · latest December 2, 1992

Counted from padside's own launch record, the same basis as the stats page.

Flights per year

  • Successful
  • Failed
Show the numbers for Molniya 8K78M-PVB flights per year
Molniya 8K78M-PVB flights per year
YearSuccessfulFailedTotal
1990303
1991000
1992505

Flights

5 of 8

All 8 flights