Zenit-2M

Last updated
  1. Krebs, Gunter. "Zenit-2SLB / Zenit-2M". Gunter's Space Page. Retrieved 2016-05-16.
  2. Krebs, Gunter. "Zenit-2FG". Gunter's Space Page. Retrieved 2016-05-16.
  3. 1 2 "Zenit-2SB". Roscosmos (in Russian). Retrieved 7 April 2016.[ permanent dead link ]
  4. "Spaceflight Now | Breaking News | Ukrainian Zenit rocket makes its return to flight".
Zenit-2M/2SB/2SLB
Zenit-2SLB.svg
Zenit-2M
Function Carrier rocket
Manufacturer Yuzhmash
Country of originFlag of Ukraine.svg  Ukraine
Size
Height57.35 metres (188.2 ft)
Diameter3.9 metres (13 ft)
Mass458,900 kilograms (1,011,700 lb)
StagesTwo
Capacity
Payload to LEO
Mass12,030 kilograms (26,520 lb)
Associated rockets
Family Zenit
Derivative work Zenit-3SLB
Zenit-3SLBF
Launch history
StatusRetired
Launch sites Baikonur Site 45/1
Total launches2 [1] [2]
Success(es)2
First flight29 June 2007
Last flight8 November 2011
First [3] stage
Height32.9 m (108 ft)
Diameter3.9 m (13 ft)
Empty mass27,564 kg (60,768 lb)
Gross mass354,350 kg (781,210 lb)
Propellant massRG-1: 90,219 kg (198,899 lb)
LOX: 236,567 kg (521,541 lb)
Powered by RD-171
Maximum thrustSea 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 time140-150 seconds
Propellant LOX/RG-1