Zenit-3F

Last updated
Zenit-3F.png
Function Carrier rocket
Manufacturer Yuzhmash
Country of originUkraine
Size
Height59.6 metres (196 ft)
Diameter3.9 metres (13 ft)
Mass471,000 kilograms (1,038,000 lb)
StagesThree
Capacity
Payload to GTO
Mass4,000 kilograms (8,800 lb) [1]
Associated rockets
Family Zenit
Launch history
StatusRetired
Launch sites Baikonur Site 45/1
First flight20 January 2011 (Elektro-L No.1)
Last flight26 December 2017 (AngoSat 1)
First stage – Zenit-2SB First stage [2]
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
Flight No.Date and time (UTC)PayloadOrbitOutcome
120 January 2011
12:29
Elektro-L No.1 GEOSuccess
218 July 2011
02:31
Spektr-R HEO Success
311 December 2015
13:45
Elektro-L No.2 GEOSuccess
426 December 2017
19:00
AngoSat 1 GEOSuccess
References: [4]

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References

  1. "Zenit-3SLBF". Yuzhnoye.
  2. 1 2 "Zenit-2SB". Roscosmos (in Russian). Retrieved 7 April 2016.
  3. "Russia meteo satellite Electro-L successfully orbited". ITAR-TASS. 2011-01-21. Archived from the original on 2011-01-22.
  4. Krebs, Gunter. "Zenit family". Gunter's Space Page. Retrieved 2009-04-15.