Movatterモバイル変換

Zenit-3F

From Wikipedia, the free encyclopedia

Expendable carrier rocket

Size

Function	Carrier rocket
Manufacturer	Yuzhmash
Country of origin	Ukraine
Height	59.6 m (196 ft)
Diameter	3.9 m (13 ft)
Mass	471,000 kg (1,038,000 lb)
Stages	3
Capacity
Payload toGTO
Mass	4,000 kg (8,800 lb)^[1]

Associated rockets
Family	Zenit
Launch history
Status	Retired
Launch sites	Baikonur,Site 45/1
First flight	20 January 2011(Elektro-L No.1)
Last flight	26 December 2017(AngoSat 1)

First stage – Zenit-2SB first stage^[2]
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	1 ×RD-171
Maximum thrust	SL: 7,257 kN (1,631,000 lb_f) vac: 7,908 kN (1,778,000 lb_f)
Specific impulse	SL: 309.5 s (3.035 km/s) vac: 337.2 s (3.307 km/s)
Burn time	140–150 seconds
Propellant	LOX/RG-1
Second stage – Zenit-2SB second stage^[2]
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 kN (205,000 lb_f) RD-8: 79.4 kN (17,800 lb_f)
Specific impulse	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 –Fregat-SB
Powered by	1 ×S5.92
Maximum thrust	19.6 kN (4,400 lb_f)
Specific impulse	327 s (3.21 km/s)
Burn time	877 seconds
Propellant	N₂O₄ /UDMH

[edit on Wikidata]

TheZenit-3F,Zenit-3SLBF orZenit-2SB/Fregat was anexpendable carrier rocket. It was a member of theZenit family of rockets, which were designed byYuzhnoye Design Bureau ofUkraine.

Launches of Zenit-3SLBF rockets were conducted fromBaikonur Cosmodrome Site 45/1. The rocket consisted of a Zenit-2SB (Zenit-2M) core vehicle, with aFregat-SB upper stage, developed by NPOLavochkin of Russia, in place of theBlock-DM used on theZenit-3SL and3SLB.

The first launch of a Zenit-3F took place on 20 January 2011. The payload was anElektro-L new generation weather satellite.^[3] A Zenit-3F was also used to successfully launch theSpektr-R radio astronomy satellite on 18 July 2011.

Launches

[edit]

Main article:List of Zenit launches

Flight No.	Date and time (UTC)	Payload	Orbit	Outcome
1	20 January 2011 12:29	Elektro-L No.1	GEO	Success
2	18 July 2011 02:31	Spektr-R	HEO	Success
3	11 December 2015 13:45	Elektro-L No.2	GEO	Success
4	26 December 2017 19:00	AngoSat 1	GEO	Success
References:^[4]

References

[edit]

^"Zenit-3SLBF". Yuzhnoye.
^^a ^b"Zenit-2SB".Roscosmos (in Russian). Retrieved7 April 2016.
^"Russia meteo satellite Electro-L successfully orbited". ITAR-TASS. 2011-01-21. Archived fromthe original on 2011-01-22.
^Krebs, Gunter."Zenit family". Gunter's Space Page. Retrieved2009-04-15.

v t e Ukrainian launch vehicles
Cyclone (Tsyklon)	Tsyklon-1M Tsyklon-2 Tsyklon-3 Tsyklon-4 Cyclone-4M
Zenit	Zenit-2 Zenit-2M Zenit-3SL Zenit-3SLB Zenit-3F
Mayak	Mayak
Dnipro (Dnepr)	Dnipro
International projects	Antares VEGA Skyrora Firefly Aerospace
Space agency

v t e Orbital launch systems
List of orbital launch systems Comparison of orbital launch systems
Current	Angara 1.2 A5 Ariane 6 Atlas V Ceres 1 1S Chollima-1 Electron Falcon 9 Block 5 Falcon Heavy Firefly Alpha Gravity-1 GSLV H-IIA H3 Hyperbola-1 Jielong 1 3 KAIROS^† Kaituozhe 2 Kinetica 1 Kuaizhou 1 1A 11 Long March 2C 2D 2F 3A 3B/E 3C 4B 4C 5 5B 6 6A 6C 7 7A 8 11 11H 12 LVM3 Minotaur I IV V C New Glenn Nuri OS-M1^† Pegasus XL Proton-M PSLV Qaem 100 Qased Shavit 2 Simorgh SLS Block 1 Soyuz-2 2.1a / STA 2.1b / STB Spectrum^† SSLV Starship Tianlong-2 Unha Vega C Vulcan Centaur Zhuque 2
In development	Antares 330 Bloostar Blue Whale 1 Cyclone-4M Deca Epsilon S Eris Gravity-2 HANBIT-NANO Hyperbola-2 Irtysh KSLV-III Kuaizhou 21 31 Long March 9 10 Miura 5 MLV Neutron New Line 1 NGLV Nova OS-M 2 4 Orbex Prime Pallas-1 Red Dwarf RFA One SLS Block 1B Block 2 Soyuz-7 Terran R Tianlong-3 VLM Vega E Zero Zhuque 3 Zuljanah
Retired	Antares 110 120 130^† 230 230+ Ariane 1 2 3 4 5 ASLV Athena I II Atlas B D E/F G H I II III LV-3B SLV-3 Able^† Agena Centaur Black Arrow Conestoga^† Delta A B C D E G J L M N 0100 1000 2000 3000 4000 5000 II III IV IV Heavy Diamant Dnepr Energia Epsilon Europa I^† II^† Falcon 1 Falcon 9 v1.0 v1.1 v1.2 "Full Thrust" Feng Bao 1 GSLV Mk I H-I H-II H-IIB Juno I Juno II Kaituozhe-1 Kosmos original 1 2/2I 3 3M Lambda 4S LauncherOne Long March 1 1D^† 2A 2E 3 3B 4A Mu 4S 3C 3H 3S 3SII V N1^† N-I N-II Naro-1 Paektusan^† Pilot-2^† R-7 Luna Molniya M L Polyot Soyuz original FG L M U U2 2-1v Soyuz/Vostok Sputnik Voskhod Vostok L K 2 2M R-29 Shtil' Volna^† Rocket 3 RS1^† Safir 1 1A 1B Saturn I IB V Scout X-1 Blue Scout II^† X-2^† X-2M X-3 X-3M X-4 X-2B^† B A B-1 D-1 A-1 E-1 F-1 G-1 Shavit original 1 SLV Space Shuttle SPARK^† Sparta SS-520 Start-1 Terran 1^† Thor Able Ablestar 1 2 Agena A B D Burner 1 2 Delta DSV-2U Thorad-Agena SLV-2G SLV-2H Titan II GLV IIIA IIIB IIIC IIID IIIE 34D 23G CT-3 IV Tsyklon R-36-O original 2 3 Universal Rocket UR-500 Proton Proton-K Rokot Strela Vanguard Vega original VLS-1^† Zenit 2 2M 2FG 3SL 3SLB 3F Zhuque 1^†
Classes	Sounding rocket Small-lift launch vehicle Medium-lift launch vehicle Heavy-lift launch vehicle Super heavy-lift launch vehicle
This template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future Symbol^† indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)

This rocketry article is astub. You can help Wikipedia byexpanding it.

Retrieved from "https://en.wikipedia.org/w/index.php?title=Zenit-3F&oldid=1259624562"

Categories:

Hidden categories:

[8]ページ先頭