Function | Carrier rocket |
---|---|
Manufacturer | Yuzhmash |
Country of origin | Ukraine |
Size | |
Height | 59.6 metres (196 ft) |
Diameter | 3.9 metres (13 ft) |
Mass | 471,000 kilograms (1,038,000 lb) |
Stages | Three |
Capacity | |
Payload to GTO | |
Mass | 3,750 kilograms (8,270 lb) |
Associated rockets | |
Family | Zenit |
Comparable | Zenit-3SLBF |
Launch history | |
Status | Active |
Launch sites | Baikonur Site 45/1 |
Total launches | 6 |
Success(es) | 6 |
First flight | 28 April 2008 (AMOS-3) |
Last flight | 31 August 2013 (AMOS-4) |
First stage – Zenit-2SB First stage [1] | |
Height | 32.9 m (108 ft) |
Diameter | 3.9 m (13 ft) |
Empty mass | 27,564 kg (60,768 lb) |
Gross mass | 354,350 kg (781,210 lb) |
Propellant mass | RG-1: 90,219 kg (198,899 lb) LOX: 236,567 kg (521,541 lb) |
Powered by | RD-171 |
Maximum thrust | Sea 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 time | 140-150 seconds |
Propellant | LOX/RG-1 |
Second stage –Zenit-2SB Second stage [1] | |
Height | 10.4 m (34 ft) |
Diameter | 3.9 m (13 ft) |
Empty mass | 8,307 kg (18,314 lb) |
Gross mass | 90,794 kg (200,167 lb) |
Propellant mass | RG-1: 23,056 kg (50,830 lb) LOX:59,431 kg (131,023 lb) |
Powered by | 1 RD-120 1 RD-8 |
Maximum thrust | RD-120: 912 kilonewtons (205,000 lbf) RD-8: 79.4 kilonewtons (17,800 lbf) |
Specific impulse | Vacuum: RD-120: 350 s (3.4 km/s) RD-8: 342.8 s (3.362 km/s) |
Burn time | 360-370 seconds |
Propellant | LOX/RG-1 |
Third stage –Blok DM-SLB | |
Powered by | 1 RD-58M |
Maximum thrust | 84.9 kilonewtons (19,100 lbf) |
Specific impulse | 352 sec |
Burn time | 650 seconds |
Propellant | LOX/RG-1 |
The Zenit 3SLB or Zenit-3M is a Ukrainian expendable carrier rocket derived from the Zenit-2SB. It is a member of the Zenit family of rockets,which were designed by the Yuzhnoye Design Office. Produced at Yuzhmash,the rocket is a modified version of the Zenit-3SL,designed to be launched from a conventional launch pad rather than the Sea Launch Ocean Odyssey platform. Most of components of the rocket are produced in Russia.
Launches of Zenit-3SLB rockets are conducted from Site 45/1 at the Baikonur Cosmodrome. Commercial launches are conducted by Land Launch,and use the designation 3SLB,whilst launches conducted by Federal Space Agency Roskosmos or the Russian Space Forces will use the designation 3M.
It consists of a Zenit 2SB (Zenit-2M) core vehicle,with a Block DM-SLB upper stage by RSC Energia (Russia). The rocket's fairing is developed by Lavochkin (Khimki,Moscow,Russia).
The launch services are provided by "Land Launch",a subsidiary of Sea Launch,and Space International Services,a Russian/Ukrainian joint venture.
The first launch of a Zenit-3SLB occurred on 28 April 2008,carrying the Israeli AMOS-3 satellite. This was also the first commercial Zenit launch from Baikonur since a failed Globalstar launch in 1998,and the first launch to be conducted by the Land Launch consortium.
Flight No. | Date and Time(UTC) | Payload | Orbit | Outcome |
---|---|---|---|---|
1 | April 28, 2008 | AMOS-3 | GEO | Success [2] |
2 | February 26, 2009 | Telstar 11N | GTO | Success [3] |
3 | June 21, 2009 | MEASAT-3a | GTO | Success [4] |
4 | November 30, 2009 | Intelsat 15 | GTO | Success [5] |
5 | October 5, 2011 | Intelsat 18 | GTO | Success |
6 | August 31, 2013 | AMOS-4 | GTO | Success |
References: [6] |
Sea Launch was a multinational—Norway, Russia, Ukraine, United States—spacecraft launch company founded in 1995 that provided orbital launch services from 1999–2014. The company used a mobile maritime launch platform for equatorial launches of commercial payloads on specialized Zenit-3SL rockets from a former mobile/floating oil drilling rig renamed Odyssey.
Zenit is a family of space launch vehicles designed by the Yuzhnoye Design Bureau in Dnipro, Ukraine, which was then part of the Soviet Union. Zenit was originally built in the 1980s for two purposes: as a liquid rocket booster for the Energia rocket and, equipped with a second stage, as a stand-alone middle-weight launcher with a payload greater than the 7 tonnes of the Soyuz but smaller than the 20 tonnes payload of the Proton. The last rocket family developed in the USSR, the Zenit was intended as an eventual replacement for the dated Soyuz and Proton families, and it would employ propellants which were safer and less toxic than the Proton's nitrogen tetroxide/UDMH mix. Zenit was planned to take over crewed spaceship launches from Soyuz, but these plans were abandoned after the dissolution of the Soviet Union in 1991.
The Tsyklon, GRAU index 11K67, was a Soviet-designed expendable launch system, primarily used to put Cosmos satellites into low Earth orbit. It is based on the R-36 intercontinental ballistic missile designed by Mikhail Yangel and made eight launches, with seven successes and one failure. All of its launches were conducted from LC-90 at the Baikonur Cosmodrome. It is sometimes designated Tsyklon-2A, not to be confused with the later Tsyklon-2 rocket. It was introduced in 1967 and was derived from the R-36 ICBM. It was retired in 1969.
The Dnepr rocket was a space launch vehicle named after the Dnieper River. It was a converted ICBM used for launching artificial satellites into orbit, operated by launch service provider ISC Kosmotras. The first launch, on April 21, 1999, successfully placed UoSAT-12, a 350 kg demonstration mini-satellite, into a 650 km circular Low Earth orbit.
The State Space Agency of Ukraine is the Ukrainian government agency responsible for space policy and programs. Along with the Ukrainian Defense Industry and the Antonov Aeronautical Scientific-Technical Complex, it is a major state complex of the national defense industry of Ukraine.The agency was formed in 1992 based on the Soviet space program infrastructure remaining in Ukraine following the dissolution of the Soviet Union.
Zenit was a series of military photoreconnaissance satellites launched by the Soviet Union between 1961 and 1994. To conceal their nature, all flights were given the public Kosmos designation.
The Zenit-2M, Zenit-2SB, Zenit-2SLB or Zenit-2FG was a Ukrainian expendable carrier rocket derived from the Zenit-3SL. It was a member of the Zenit family of rockets, which were designed by the Yuzhmash.
Land Launch refers to a service product of Sea Launch SA. There is no entity or company called Land Launch. Sea Launch created the Land Launch offering to address lighter satellites directly into geosynchronous orbit or into geosynchronous transfer orbit, while Sea Launch continues to address the heavy satellite launch market.
AsiaSat 5 is a Hong Kong communications satellite, which is operated by the Hong Kong based Asia Satellite Telecommunications Company (AsiaSat). It is positioned in geostationary orbit at a longitude of 100.5° East of the Greenwich Meridian, where it replaced the AsiaSat 2 satellite. It is used to provide fixed satellite services, including broadcasting, telephone and broadband very small aperture terminal (VSAT) communications, to Asia and the Pacific Ocean region.
The Zenit-2 is a Ukrainian, previously Soviet, expendable carrier rocket. First flown in 1985, it has been launched 37 times, with 6 failures. It is a member of the Zenit family of rockets and was designed by the Yuzhmash.
AMOS-3, also known as AMOS-60, is an Israeli communications satellite operated by Spacecom Satellite Communications.
MEASAT-3a is a communications satellite which MEASAT Satellite Systems intends to operate in geosynchronous orbit at 91.5 degrees East longitude. It was built by Orbital Sciences Corporation, based on the STAR-2 spacecraft platform.
Site 45 at the Baikonur Cosmodrome is a launch site used by Zenit rockets. It consists of two pads, one of which is still in use. It has been the launch site for all Soviet and Russian government Zenit launches, along with a commercial launch conducted for Globalstar in 1998, and continuing commercial launches under the Land Launch programme. The main pad at the site is area 45/1, which was completed in 1983 following five years of construction. A second pad, area 45/2, was completed in 1990, but was destroyed by a launch failure in the same year.
The Zenit-3F, Zenit-3SLBF or Zenit-2SB/Fregat is an expendable carrier rocket. It is a member of the Zenit family of rockets, which were designed by Yuzhnoye Design Bureau of Ukraine.
Intelsat 15, also known as IS-15, is a communications satellite owned by Intelsat. Intelsat 15 was built by Orbital Sciences Corporation, on a Star-2.4. It is located at 85° E longitude on the geostationary orbit. It was launched from Baikonur Cosmodrome to a geosynchronous transfer orbit on 30 November 2009 by a Zenit-3SLB launch vehicle. It has 22 active Ku band transponders, plus eight spares. Five of those transponders are owned and operated by SKY Perfect JSAT Group under the name JCSAT-85.
Elektro–L is a series of meteorological satellites developed for the Russian Federal Space Agency by NPO Lavochkin. The first satellite, Elektro-L No.1, was launched on 2 January 2011. It is the first Russian weather satellite that successfully operates in geostationary orbit, and is currently the second operational Russian weather satellite. The satellites have a mass of about 1620 kg and are designed to operate for 10 years each. They are capable of producing images of the Earth's whole hemisphere in both visible and infrared frequencies, providing data for climate change and ocean monitoring in addition to their primary weather forecasting role.
AMOS-4 is an Israeli commercial communications satellite, operated by Spacecom Satellite Communications, Tel Aviv-based, part of the AMOS series of satellites.
AngoSat 1 was a geostationary communications satellite operated by Angosat and built by the Russian company RKK Energia. It was the first communications satellite of Angola, designed for a 15-year mission to deliver television, internet, and radio services to Angola and other territories. The satellite suffered a power problem in the first hours of flight and lost contact with ground control. After the power problem, contact was established with the satellite, but ultimately the satellite did not recover, and contact was lost permanently 3 days into the mission. After repeated failures to establish contact in the following weeks/months, the satellite was declared lost. Russia built a replacement satellite AngoSat 2.
Irtysh, also named Soyuz-5, formerly codenamed Fenix in Russian and Sunkar in Kazakh, is a planned Russian rocket that is being developed by JSC SRC Progress within the "Project Feniks". Initially it will replace the capability of Zenit-2 and Proton Medium, and in the future will serve as the base of a super heavy-lift launch vehicle rocket (Yenisei) to match the Energia/Buran capabilities. As of February 2021, Irtysh is expected to launch from the Baikonur Baiterek, the ex Zenit-2 launch site, in a partnership with the government of Kazakhstan, with a planned debut in late 2023.