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Zenit-2M

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Zenit-2M/2SB/2SLB
Zenit-2M
FunctionCarrier rocket
ManufacturerYuzhmash
Country of originUkraine
Size
Height57.35 metres (188.2 ft)
Diameter3.9 metres (13 ft)
Mass458,900 kilograms (1,011,700 lb)
StagesTwo
Capacity
Payload toLEO
Mass12,030 kilograms (26,520 lb)
Associated rockets
FamilyZenit
Derivative workZenit-3SLB
Zenit-3SLBF
Launch history
StatusRetired
Launch sitesBaikonurSite 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 byRD-171
Maximum thrustSea Level:7,257 kN (1,631,000 lbf)
Vacuum:7,908 kN (1,778,000 lbf)
Specific impulseSea Level:309.5 s (3.035 km/s)
Vacuum:337.2 s (3.307 km/s)
Burn time140-150 seconds
PropellantLOX/RG-1
Second[3]stage
Height10.4 m (34 ft)
Diameter3.9 m (13 ft)
Empty mass8,307 kg (18,314 lb)
Gross mass90,794 kg (200,167 lb)
Propellant massRG-1:23,056 kg (50,830 lb)
LOX:59,431 kg (131,023 lb)
Powered by1RD-120
1RD-8
Maximum thrustRD-120:912 kilonewtons (205,000 lbf)
RD-8:79.4 kilonewtons (17,800 lbf)
Specific impulseVacuum:
RD-120:350 s (3.4 km/s)
RD-8:342.8 s (3.362 km/s)
Burn time360-370 seconds
PropellantLOX/RG-1

TheZenit-2M,Zenit-2SB,Zenit-2SLBorZenit-2FGwas aUkrainianexpendablecarrier rocketderived from theZenit-3SL.It was a member of theZenitfamily ofrockets,which were designed by theYuzhmash.

Development[edit]

The Zenit 2M was a modernised version of theZenit-2,incorporating modifications and upgrades made to the design for theSea Launchprogramme.

Launches of Zenit-2M rockets were conducted fromBaikonur CosmodromeSite 45/1.Commercial launches are conducted byLand Launch,and use the designation 2SLB, however as of 2011, no commercial launches have been ordered and no launch of 2SLB has taken place as of 2023. Launches conducted byRoskosmosor theRussian Space Forcesuse the designation 2M. The designation 2SB can also be applied to the rocket when it is being used as part of a larger vehicle, such as theZenit-3SLB.

The first launch of a Zenit-2M occurred on 29 June 2007, carrying the lastTselina-2ELINTsatellite for theRussian Space Forces,Tselina-2 satellites having been previously launched by older Zenit-2 rockets.[4]The second launch, carrying theFobos-GruntandYinghuo-1spacecraft, was conducted on 8 November 2011, using a modified configuration designated theZenit-2FG.This configuration incorporated the payload fairing used on theZenit-3Frocket, and a special adaptor for the Fobos-Grunt spacecraft, which incorporated aFregat-derived propulsion system. The Zenit-2 and Zenit-2M, however, were supplanted by theZenit-3SLBafter 2008.

See also[edit]

References[edit]

  • Wade, Mark."Zenit".Encyclopedia Astronautica.Archived fromthe originalon August 28, 2003.Retrieved2009-04-15.
  • Krebs, Gunter."Zenit family".Gunter's Space Page.Retrieved2009-04-15.
  1. ^Krebs, Gunter."Zenit-2SLB / Zenit-2M".Gunter's Space Page.Retrieved2016-05-16.
  2. ^Krebs, Gunter."Zenit-2FG".Gunter's Space Page.Retrieved2016-05-16.
  3. ^ab"Zenit-2SB".Roscosmos(in Russian).Retrieved7 April2016.
  4. ^"Spaceflight Now | Breaking News | Ukrainian Zenit rocket makes its return to flight".