Zenit-3SL

Zenit-3SL
Function	Carrier rocket
Manufacturer	Yuzhmash (Zenit) RKK Energia (Block-DM) Boeing (fairing)
Country of origin	Ukraine
Size
Height	59.6 metres (196 ft)
Diameter	3.9 metres (13 ft)
Mass	462,200 kilograms (1,019,000 lb)
Stages	Three
Capacity
Payload to GTO
Mass	6,160 kilograms (13,580 lb)[1]
Associated rockets
Family	Zenit
Derivative work	Zenit-3SLB
Launch history
Status	Retired
Launch sites	Ocean Odyssey
Total launches	36
Success(es)	32
Failure(s)	3
Partial failure(s)	1
First flight	28 March 1999 (test flight)
Last flight	26 May 2014 (Eutelsat 3B)
First stage
Powered by	1 RD-171
Maximum thrust	8,180 kilonewtons (1,840,000 lbf)
Specific impulse	337 sec
Burn time	150 seconds
Propellant	RP-1/LOX
Second stage
Powered by	1 RD-120 1 RD-8
Maximum thrust	912 kilonewtons (205,000 lbf) 79.5 kilonewtons (17,900 lbf)
Specific impulse	349 sec
Burn time	315 seconds
Propellant	RP-1/LOX
Third stage – Block DM-SL
Powered by	1 RD-58M
Maximum thrust	84.9 kilonewtons (19,100 lbf)
Specific impulse	352 sec
Burn time	650 seconds
Propellant	RP-1/LOX
[edit on Wikidata]

The Zenit-3SL was an expendable carrier rocket operated by Sea Launch. First flown in 1999,^[2] 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.^[3] 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.

The Zenit-3SL design began in the late 1980s as the Zenit-3, a proposed replacement for the Proton-K, which would have used a Zenit-2 rocket with a Block D upper stage. This proposal was shelved after the dissolution of the Soviet Union, as Russia inherited the space programme, however the Zenit was manufactured in Ukrainian SSR. Boeing became involved in the programme in 1994. The design was subsequently modified, with a modified version of the Block DM replacing the Block D.^[2][4]

Sea Launch integrated the rockets in California, and transfers them to Odyssey via the Sea Launch Commander for transportation to the launch site. Once at the launch site, the rocket was erected on the platform, and a three-day countdown was initiated. The countdown was fully automated,^[5] and personnel were evacuated from the launch platform to Commander prior to launch.

Zenit-3SL launches predominantly carried communications satellites into geosynchronous transfer orbits. As of 2009, the only payload to be launched by a Zenit-3SL that was not a communications satellite was a DemoSat, on the maiden flight. The only launch to be conducted to an orbit other than GTO was that of ICO F-1, which was intended to be placed into medium Earth orbit, however the rocket failed to reach orbit.