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Zenit-3F - Revision history
2026-11-14T18:35:08Z
Revision history for this page on the wiki
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CallGirlMumbai: update
2026-02-17T11:42:37Z
<p>update</p>
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CallGirlMumbai
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Jaesingh: Created page with "{{Infobox Rocket |image = Zenit-3F.png |image_size = 40 |function = Carrier rocket |manufacturer = Yuzhmash |country-origin = Ukraine |height..."
2021-06-09T20:25:56Z
<p>Created page with "{{Infobox Rocket |image = Zenit-3F.png |image_size = 40 |function = <a href="/w/index.php?title=Carrier_rocket&action=edit&redlink=1" class="new" title="Carrier rocket (page does not exist)">Carrier rocket</a> |manufacturer = <a href="/w/index.php?title=Yuzhmash&action=edit&redlink=1" class="new" title="Yuzhmash (page does not exist)">Yuzhmash</a> |country-origin = Ukraine |height..."</p>
<p><b>New page</b></p><div>{{Infobox Rocket<br />
|image = Zenit-3F.png<br />
|image_size = 40<br />
|function = [[Carrier rocket]]<br />
|manufacturer = [[Yuzhmash]]<br />
|country-origin = Ukraine<br />
|height = {{convert|59.6|m}}<br />
|diameter = {{convert|3.9|m}}<br />
|mass = {{convert|471000|kg}}<br />
|stages = Three<br />
|capacities =<br />
{{Infobox Rocket/Payload<br />
|location = [[Geostationary transfer orbit|GTO]]<br />
|kilos = {{convert|4000|kg}}<ref>{{cite web|title=Zenit-3SLBF|publisher=Yuzhnoye|url=https://yuzhnoye.com.ua/pervyy-pusk-zenita}}</ref><br />
}}<br />
|family = [[Zenit (rocket family)|Zenit]]<br />
|status = Active<br />
|first = 20 January 2011 ([[Elektro-L No.1]])<br />
|last = 26 December 2017 ([[AngoSat 1]])<br />
|sites = [[Baikonur Cosmodrome|Baikonur]] [[Baikonur Cosmodrome Site 45|Site 45/1]]<br />
|stagedata = <!--insert one of the following templates for each stage:--><br />
{{Infobox rocket/stage<br />
|type = stage<br />
|diff = <!--variant of rocket this is used on, optional--><br />
|stageno = First<br />
|name = Zenit-2SB First stage<ref name="Roscosmos-Zenit-2SB">{{cite web|title=Zenit-2SB|url=http://www.federalspace.ru/475/|website=Roscosmos|access-date=7 April 2016|language=ru}}</ref><br />
|number = <!--number of boosters, required if type = booster--><br />
|length = {{convert|32.9|m|ft|abbr=on}}<br />
|diameter = {{convert|3.9|m|ft|abbr=on}}<br />
|width = <!--width of a single booster/stage if not axisymmetric, use {{convert|WIDTH|m|abbr=on}}, optional--><br />
|empty = {{convert|27564|kg|lb|abbr=on}}<br />
|gross = {{convert|354350|kg|lb|abbr=on}}<br />
|propmass = '''RG-1:''' {{convert|90219|kg|lb|abbr=on}}<br/>'''LOX: '''{{convert|236567|kg|lb|abbr=on}}<br />
|engines = [[RD-171]]<!--number and type of engines used on each individual booster/stage, required--><br />
|solid = <!--set to "yes" (lowercase) to change Engines to Motor for solid motors--><br />
|thrust = '''Sea Level:''' {{convert|7257|kN|lbf|abbr=on}}<br/>'''Vacuum:''' {{convert|7908|kN|lbf|abbr=on}}<br />
|total = <!--total thrust for all boosters in kN, use {{convert|THRUST|kN|abbr=on}}, optional--><br />
|SI = '''Sea Level:''' {{convert|309.5|isp|abbr=on}}<br/>'''Vacuum:''' {{convert|337.2|isp|abbr=on}}<br />
|burntime = 140-150 seconds<br />
|fuel = [[LOX]]/[[RG-1 (propellant)|RG-1]]<br />
}}<br />
{{Infobox rocket/stage<br />
|type = stage<br />
|diff = <!--variant of rocket this is used on, optional--><br />
|stageno = Second<br />
|name = Zenit-2SB Second stage<ref name="Roscosmos-Zenit-2SB" /><br />
|number = <!--number of boosters, required if type = booster--><br />
|length = {{convert|10.4|m|ft|abbr=on}}<br />
|diameter = {{convert|3.9|m|ft|abbr=on}}<br />
|width = <!--width of a single booster/stage if not axisymmetric, use {{convert|WIDTH|m|abbr=on}}, optional--><br />
|empty = {{convert|8307|kg|lb|abbr=on}}<br />
|gross = {{convert|90794|kg|lb|abbr=on}}<br />
|propmass = '''RG-1:''' {{convert|23056|kg|lb|abbr=on}}<br/>'''LOX: '''{{convert|59431|kg|lb|abbr=on}}<br />
|engines = 1 [[RD-120]]<br/>1 [[RD-8]]<!--number and type of engines used on each individual booster/stage, required--><br />
|solid = <!--set to "yes" (lowercase) to change Engines to Motor for solid motors--><br />
|thrust = '''RD-120:''' {{convert|912|kN}}<br/>'''RD-8:''' {{convert|79.4|kN}}<br />
|total = <!--total thrust for all boosters in kN, use {{convert|THRUST|kN|abbr=on}}, optional--><br />
|SI = '''Vacuum:'''<br/>'''RD-120:''' {{convert|350|isp|abbr=on}}<br/>'''RD-8:''' {{convert|342.8|isp|abbr=on}}<br />
|burntime = 360-370 seconds<br />
|fuel = [[LOX]] / [[RG-1 (propellant)|RG-1]]<br />
}}<br />
{{Infobox rocket/stage<br />
|type = stage<br />
|diff = <!--variant of rocket this is used on, optional--><br />
|stageno = Third<br />
|name = [[Fregat|Fregat-SB]]<br />
|engines = 1 [[S5.92]]<br />
|thrust = {{convert|19.6|kN}}<br />
|SI = 327 s<br />
|burntime = 877 s<br />
|fuel = [[dinitrogen tetraoxide]] / [[UDMH]]<br />
}}<br />
}}<br />
<br />
The '''Zenit-3F''', '''Zenit-3SLBF''' or '''Zenit-2SB/Fregat''' is an [[expendable launch system|expendable]] [[carrier rocket]]. It is a member of the [[Zenit (rocket family)|Zenit]] family of rockets, which were designed by [[Yuzhnoye Design Bureau]] of [[Ukraine]].<br />
<br />
Launches of Zenit-3SLBF rockets are conducted from [[Baikonur Cosmodrome Site 45|Baikonur Cosmodrome Site 45/1]]. The rocket consists of a Zenit-2SB (Zenit-2M) core vehicle, with a [[Fregat|Fregat-SB]] upper stage, developed by NPO [[Lavochkin]] of Russia, in place of the [[Blok D|Block-DM]] used on the [[Zenit-3SL]] and [[Zenit-3SLB|3SLB]].<br />
<br />
The first launch of a Zenit-3F took place on 20 January 2011. The payload was an [[Elektro-L]] new generation weather satellite.<ref name="itartass_launch">{{cite web|url=http://www.itar-tass.com/eng/level2.html?NewsID=15877644|title=Russia meteo satellite Electro-L successfully orbited|publisher=ITAR-TASS|date=2011-01-21|url-status=dead|archive-url=https://www.webcitation.org/5vw1LNgQr?url=http://www.itar-tass.com/eng/level2.html?NewsID=15877644&PageNum=0|archive-date=2011-01-22}}</ref> A Zenit-3F was also used to successfully launch the [[Spektr-R]] radio astronomy satellite on 18 July 2011.<br />
<br />
==Launches==<br />
{{Main|List of Zenit launches}}<br />
{| class="wikitable sortable" border="1"<br />
|-<br />
! Flight No.<br />
! Date and time ([[UTC]])<br />
! Payload<br />
! Orbit<br />
! Outcome<br />
|-<br />
!| 1<br />
| 20 January 2011<br/>12:29<br />
| [[Elektro-L No.1]]<br />
| GEO<br />
| {{Success}}<br />
|-<br />
!| 2<br />
| 18 July 2011<br/>02:31<br />
| [[Spektr-R]]<br />
| [[High Earth orbit|HEO]]<br />
| {{Success}}<br />
|-<br />
!| 3<br />
| 11 December 2015<br/>13:45<br />
| [[Elektro-L No.2]]<br />
| GEO<br />
| {{Success}}<br />
|-<br />
!| 4<br />
| 26 December 2017<br/>19:00<br />
| [[AngoSat 1]]<br />
| GEO<br />
| {{Success}}<br />
|-<br />
| colspan="5" style="text-align: left;"|'''References:'''<ref>{{cite web|url=http://space.skyrocket.de/doc_lau_fam/zenit.htm|title=Zenit family|first=Gunter|last=Krebs|publisher=Gunter's Space Page|access-date=2009-04-15}}</ref><br />
|}<br />
<br />
==References==<br />
{{reflist}}<br />
<br />
{{Ukrainian launch vehicles|state=expanded}}<br />
{{expendable launch systems}}<br />
<br />
<br />
{{rocket-stub}}<br />
<br />
[[Category:Zenit (rocket family)]]<br />
[[Category:Vehicles introduced in 2011]]</div>
Jaesingh