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    The Zenit rocket (Ukrainian: Зеніт, Russian: Зени́т; meaning Zenith) is a space launch vehicle manufactured by the Yuzhnoe Design Bureau of Ukraine. Zenit was 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 rocket. Moreover Zenit was planned to take over manned spaceship launches from Soyuz, but these plans were abandoned after the fall of the Soviet Union.

    Zenits are launched from Russia's Baikonur Cosmodrome in Kazakhstan, and by the Sea Launch consortium's floating launch platform in the Pacific Ocean. The engines of the Zenit's first and second stages as well as the upper stage of the Zenit-3SL rocket are supplied by Russia. Since the Zenit is not built in Russia, it is planned to be replaced in that service by the new and yet unflown Angara rocket, although Russia does still use the Zenit. There are plans to use an improved Zenit-3SLB rocket for commercial launches from Baikonur Cosmodrome beginning with 2007; this service is marketed as "Land Launch."

    In the study entitled The Military Use of Space: A Diagnostic Assessment (csbaonline.org for copies), data compiled by Greg Lucas and Charles Murphy in Appendix 4 of the study shows that among the 16 launchers surveyed, the Zenit 2 is currently the lowest cost vehicle for achieving LEO in terms of payload weight per launch ($1167-1667 per pound), and one of the lowest in terms of total costs per launch ($35-$50 million). *

    Current models:










        Zenit rocket
            Zenit 3SL
    image
    CaptionZenit-2 rocket (Baikonur, 10 December 2001)
    NameZenit
    FunctionMedium expendable Carrier rocket
    ManufacturerYuzhnoe Design Bureau
    CountryUkraine
    Height57-59.6 metre
    Alt-height187-195 foot (unit of length)
    Diameter3.9 m
    Alt-diameter12.7 ft
    Mass444,900 -462,200 kilogram
    Alt-mass1,011,700 - 1,038,000 lb pound (mass)
    Stages2 or 3
    Leo-payloadZenit 2 - 13,740 kg
    Alt-leo30,290lb
    Payload-locationSSO
    PayloadZenit 2 - 13,740 kg
    Alt-payload11,000 lb
    Payload2-locationGTO
    Payload2GTO
    Alt-payload211,570 lb
    StatusActive
    SitesLC-45, Baikonur Cosmodrome
    Ocean Odyssey
    Launches61
    37 Zenit 2
    24 Zenit 3SL
    Success53
    31 Zenit 2
    22 Zenit 3SL
    Fail8
    6 Zenit 2
    2 Zenit 3SL
    FirstZenit 2:13 April, 1985
    Zenit 3SL: 28 March...
    Last
    Stage1nameZenit
    Stage1engines1 RD-171
    Stage1thrust8.18 newton
    Alt-stage1thrust1,839,000 pound-force
    Stage1time150 seconds
    Stage1si337 sec
    Stage1fuelRP-1/LOX
    Stage2engines1 RD-120, 1RD-8
    Stage2thrust912 kN/79,5 kN
    Alt-stage2thrust205,025 lbf
    Stage2time315 seconds
    Stage2si349 sec
    Stage2fuelRP-1/LOX
    Stage3nameBlock DM-SL
    Stage3engines1 RD-58M
    Stage3thrust84.9 kN
    Alt-stage3thrust19,091 lbf
    Stage3time650 seconds
    Stage3si352 sec

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    Zenit 3SL
    Zenit-3SL is a three stage carrier rocket developed for and used by the Sea Launch consortium.

    It combines:
      nose-cone enclosure for protection of payload during launch, provided by Boeing.

    Rockets used by Sea Launch are assembled in Long Beach, California. Launches occur from the Ocean Odyssey offshore launch platform, situated at the equator. The Ocean Odyssey is also used to transport rockets to the launch site.


     
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    This article is licensed under the GNU Free Documentation License [copyleft]. It uses material from the Wikipedia article "Zenit rocket". link