Zenit-3SL

Zenit-3SL
FunctionCarrier rocket
ManufacturerYuzhmash (Zenit)
RKK Energia (Block-DM)
Boeing (fairing)
Country of originUkraine
Size
Height59.6 metres (196 ft)
Diameter3.9 metres (13 ft)
Mass462,200 kilograms (1,019,000 lb)
StagesThree
Capacity
Payload to GTO
Mass6,160 kilograms (13,580 lb)
Associated rockets
FamilyZenit
Derivative workZenit-3SLB
Launch history
StatusRetired
Launch sitesOcean Odyssey
Total launches36
Success(es)32
Failure3
Partial failure1
First flight28 March 1999 (test flight)
Last flight26 May 2014 (Eutelsat 3B)
First stage
Powered by1 RD-171
Maximum thrust8,180 kilonewtons (1,840,000 lbf)
Specific impulse337 sec
Burn time150 seconds
PropellantRP-1/LOX
Second stage
Powered by1 RD-120
1 RD-8
Maximum thrust912 kilonewtons (205,000 lbf)
79.5 kilonewtons (17,900 lbf)
Specific impulse349 sec
Burn time315 seconds
PropellantRP-1/LOX
Third stage – Block DM-SL
Powered by1 RD-58M
Maximum thrust84.9 kilonewtons (19,100 lbf)
Specific impulse352 sec
Burn time650 seconds
PropellantRP-1/LOX

The Zenit-3SL was an expendable carrier rocket operated by Sea Launch. First flown in 1999, it was launched 36 times, with three failures and one partial failure. It was a member of the Zenit family of rockets, and is built by the Yuzhnoye Design Bureau. RKK Energia produced the Block DM-SL upper stage, whilst the payload fairing was produced by Boeing. Launches were conducted from the Ocean Odyssey platform anchored on the equator in the Pacific Ocean, at a point with 154°W longitude, about 370 kilometres east of Kiritimati.