Back Зенит-2М Bulgarian Zenit-2M Galician Zenit-2M ID ゼニット2M Japanese Zenit-2M Portuguese Зенит-2М (ракета-носитель) Russian Зеніт-2SLБ Ukrainian
 Zenit-2M | |
| Function | Carrier rocket |
|---|---|
| Manufacturer | Yuzhmash |
| Country of origin |  Ukraine |
| Size | |
| Height | 57.35 metres (188.2 ft) |
| Diameter | 3.9 metres (13 ft) |
| Mass | 458,900 kilograms (1,011,700 lb) |
| Stages | Two |
| Capacity | |
| Payload to LEO | |
| Mass | 12,030 kilograms (26,520 lb) |
| Associated rockets | |
| Family | Zenit |
| Derivative work | Zenit-3SLB Zenit-3SLBF |
| Launch history | |
| Status | Retired |
| Launch sites | Baikonur Site 45/1 |
| Total launches | 2[1][2] |
| Success(es) | 2 |
| First flight | 29 June 2007 |
| Last flight | 8 November 2011 |
| First[3] stage | |
| Height | 32.9 m (108 ft) |
| Diameter | 3.9 m (13 ft) |
| Empty mass | 27,564 kg (60,768 lb) |
| Gross mass | 354,350 kg (781,210 lb) |
| Propellant mass | RG-1: 90,219 kg (198,899 lb) LOX: 236,567 kg (521,541 lb) |
| Powered by | RD-171 |
| Maximum thrust | Sea Level: 7,257 kN (1,631,000 lbf) Vacuum: 7,908 kN (1,778,000 lbf) |
| Specific impulse | Sea Level: 309.5 s (3.035 km/s) Vacuum: 337.2 s (3.307 km/s) |
| Burn time | 140-150 seconds |
| Propellant | LOX/RG-1 |
| Second[3] stage | |
| Height | 10.4 m (34 ft) |
| Diameter | 3.9 m (13 ft) |
| Empty mass | 8,307 kg (18,314 lb) |
| Gross mass | 90,794 kg (200,167 lb) |
| Propellant mass | RG-1: 23,056 kg (50,830 lb) LOX: 59,431 kg (131,023 lb) |
| Powered by | 1 RD-120 1 RD-8 |
| Maximum thrust | RD-120: 912 kilonewtons (205,000 lbf) RD-8: 79.4 kilonewtons (17,800 lbf) |
| Specific impulse | Vacuum: RD-120: 350 s (3.4 km/s) RD-8: 342.8 s (3.362 km/s) |
| Burn time | 360-370 seconds |
| Propellant | LOX/RG-1 |
The Zenit-2M, Zenit-2SB, Zenit-2SLB or Zenit-2FG was a Ukrainian expendable carrier rocket derived from the Zenit-3SL. It was a member of the Zenit family of rockets, which were designed by the Yuzhmash.
- ^ Krebs, Gunter. "Zenit-2SLB / Zenit-2M". Gunter's Space Page. Retrieved 2016-05-16.
- ^ Krebs, Gunter. "Zenit-2FG". Gunter's Space Page. Retrieved 2016-05-16.
- ^ a b "Zenit-2SB". Roscosmos (in Russian). Retrieved 7 April 2016.