Soyuz-U2
Soyuz familySoviet Space ProgramRetired
The Soyuz-U2 was a Soviet, later Russian, carrier rocket. It was derived from the Soyuz-U, and a member of the R-7 family of rockets. It featured increased performance compared with the baseline Soyuz-U, due to the use of syntin propellant, as opposed to RP-1 paraffin, used on the Soyuz-U.
Specifications
- Thrust
- 4,061 kN
- Height
- 34.54 m
- Diameter
- 2.95 m
- Launch mass
- 298 t
- Stages
- 2
- LEO capacity
- 7,050 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
71flightswith a definitive outcome
100%success rate71 of 71
71success streakcurrent
Counted from padside's own launch record, the same basis as the stats page.