Zenit is a family of space launch vehicles designed by the Yuzhnoye Design Bureau in Dnipro, Ukraine, which was then part of the Soviet Union.
Specifications
- Thrust
- 7,300 kN
- Height
- 57 m
- Diameter
- 3.9 m
- Launch mass
- 459 t
- Stages
- 2
- Launch cost
- —
- LEO capacity
- 13,740 kg
- GTO capacity
- —
- GEO capacity
- —
- SSO capacity
- 5,000 kg
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
35
Launches with a definitive outcome
Success rate
82.9%
29 of 35
Current success streak
7
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
—
Between consecutive booster flights
Counted from padside's own launch record — the same basis as the Stats page.
Launches
- Zenit-2 | Tselina-2 22 — Success
- Zenit-2 | Meteor-3M No. 1 — Success
- Zenit-2 | Orlets-2 2 — Success
- Zenit-2 | Tselina-2 21 — Success
- Zenit-2 | Okean-O — Success