Zenit-2
Zenith familyYuzhnoye Design BureauRetired
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
- LEO capacity
- 13,740 kg
- SSO capacity
- 5,000 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
35flightswith a definitive outcome
82.9%success rate29 of 35
6failuresincluding partial failures
7success streakcurrent
First flight April 13, 1985 · latest June 10, 2004
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Zenit-2 flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 1985 | 2 | 2 | 4 |
| 1986 | 2 | 0 | 2 |
| 1987 | 5 | 0 | 5 |
| 1988 | 2 | 0 | 2 |
| 1989 | 0 | 0 | 0 |
| 1990 | 1 | 1 | 2 |
| 1991 | 0 | 1 | 1 |
| 1992 | 2 | 1 | 3 |
| 1993 | 2 | 0 | 2 |
| 1994 | 4 | 0 | 4 |
| 1995 | 1 | 0 | 1 |
| 1996 | 1 | 0 | 1 |
| 1997 | 0 | 1 | 1 |
| 1998 | 2 | 0 | 2 |
| 1999 | 1 | 0 | 1 |
| 2000 | 2 | 0 | 2 |
| 2001 | 1 | 0 | 1 |
| 2002 | 0 | 0 | 0 |
| 2003 | 0 | 0 | 0 |
| 2004 | 1 | 0 | 1 |