Soyuz (rocket)

This article is about the original Soyuz rocket. For later derivatives, see Soyuz (rocket family).

Soyuz 11A511
Size
A later variant of the Soyuz rocket being rolled out to the launch pad at the Baikonur Cosmodrome in Kazakhstan.
Function	Carrier rocket
Manufacturer	OKB-1
Country of origin	USSR
Height	45.6 metres (150 ft)
Diameter	10.3 metres (34 ft)
Mass	308,000 kilograms (679,000 lb)
Stages	2
Capacity
Payload to LEO	6,450 kilograms (14,220 lb)
Associated rockets
Family	R-7 (Soyuz)
Derivatives	Soyuz-L Soyuz-M Soyuz-U
Launch history
Status	Retired
Launch sites	Baikonur Sites 1/5 & 31/6
Total launches	32^[1]
Successes	30
Failures	2
First flight	28 November 1966
Last flight	14 October 1976
Notable payloads	Soyuz

Boosters - Block A/B/V/G
No. boosters	4
Engines	1 RD-107
Thrust	994.3 kilonewtons (223,500 lbf)
Specific impulse	315 sec
Burn time	118 seconds
Fuel	RP-1/LOX
First stage - 11S59
Engines	1 RD-108
Thrust	977.7 kilonewtons (219,800 lbf)
Specific impulse	315 sec
Burn time	292 seconds
Fuel	RP-1/LOX
Second stage - 11S510
Engines	1 RD-0110
Thrust	294 kilonewtons (66,000 lbf)
Specific impulse	330 sec
Burn time	246 seconds
Fuel	RP-1/LOX

The Soyuz (Russian: Союз, meaning "union", GRAU index 11A511) was a Soviet expendable carrier rocket designed in the 1960s by OKB-1 and manufactured by State Aviation Plant No. 1 in Kuybyshev, Soviet Union. It was commissioned to launch Soyuz spacecraft as part of the Soviet human spaceflight program, first with 8 unmanned test flights, followed by the first 19 manned launches.^[1] The original Soyuz also propelled four test flights of the improved Soyuz 7K-T capsule between 1972 and 1974. In total it flew 30 successful missions over 10 years and suffered two failures.^[1]

The Soyuz 11A511 type, a member of the R-7 family of rockets. first flew in 1966. Derived from the Voskhod 11A57 type, It was a two-stage rocket, with four liquid-fuelled strap-on boosters clustered around the first stage, with a Block I second stage. The new, uprated core stage and strap-ons became standard for all R-7 derived launch vehicles to replace the numerous older variants in use on the 8A92, 11A57, and 8K78M types. While the original Blok I stage as developed in 1960 used RD-107 engines, the Soyuz boosters instead had RD-110s, which were more powerful due to the heavier weight of the Soyuz craft and also had several design improvements to increase reliability and safety on manned missions. The Molniya 8K78M booster also adopted the RD-110 during 1965, but Voskhod boosters continued using the older RD-107.^[2]

Starting in 1973, the original Soyuz rocket was gradually superseded by the Soyuz-U derivative type, which became the world's most prolific launcher, flying hundreds of missions over 43 years until its retirement scheduled for 2016. Other direct variants were Soyuz-L for low Earth orbit tests of the LK lunar lander (3 flights) and Soyuz-M built for a quickly abandoned military spacecraft and used for reconnaissance satellites instead (8 flights).

The aborted Soyuz 18-1 launch in 1975 was the final manned flight of the 11A511 and as it occurred shortly before the ASTP mission, the United States requested that the Soviets provide details about this failure. They stated that Soyuz 19 would be using the newer 11A5511U booster model (i.e. Soyuz-U) so that the Soyuz 18-1 malfunction had no bearing on it.

Soyuz rockets were assembled horizontally in the MIK Building at the launch site. The rocket was then rolled out, and erected on the launch pad.

References

Wikimedia Commons has media related to Soyuz (rocket).

1 2 3 Krebs, Gunter. "Soyuz (11A511)". Gunter's space page. Retrieved 6 May 2016.
↑ ""Soyuz" - series launch vehicles". Samara Space Centre.

Soviet, Russian, and Ukrainian launch vehicles

Active	Angara 1.2 A5 Dnepr R-7 Soyuz U FG Soyuz-2 2.1a 2.1b 2-1v UR Proton-M Rokot Strela Zenit 3SL 3SLB 3F

In development	Angara 1.1 A5P A5V Mayak L1 L2 M1 M2 H3 H5 Proton Light Medium Soyuz-5 5.1 5.2 5.3 Tsyklon-4

Retired	Energia Kosmos 1 2I 3 3M N1 Proton UR-500 Proton-K R-7 Luna Molniya M L Polyot Soyuz original L M U2 Soyuz/Vostok Sputnik Voskhod Vostok L K 2 2M R-29 Shtil' Volna Rus-M (cancelled) Start-1 Tsyklon 2 3 Zenit 2 2M

Orbital launch systems

See also: Comparison of orbital launch systems

Current	Angara 1.2 A5 Antares 200 Ariane 5 Atlas V Delta II IV Dnepr Epsilon Falcon 9 v1.2 "Full Thrust" GSLV H-IIA H-IIB Kuaizhou Long March 2C 2D 2F 3A 3B 3C 4B 4C 5 6 7 11 LVM3 Minotaur I IV V C Pegasus Proton-M PSLV Rokot Safir Shavit Simorgh Soyuz U FG Soyuz-2 2.1a / STA 2.1b / STB 2-1v Strela Unha Vega Zenit 3SL 3SLB 3F

In development	Angara A5P A5V Antares 300 Ariane 6 Electron Falcon 9 "Block 5" Falcon Heavy Firefly α H3 ITS KZ-11 KZ-21 Long March 8 9 LauncherOne Mayak Naga-L Naro-2 New Glenn Orel Proton Light Medium RPS SLS Soyuz-5 SPARK SS-520 Tronador II Tsyklon-4 ULV VLM Vulcan

Retired	Antares 100 Ariane 1 2 3 4 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 III Diamant Energia Europa Falcon 1 Falcon 9 v1.0 v1.1 Feng Bao 1 H-I H-II Juno I Juno II Kaituozhe-1 Kosmos 1 2I 3 3M Lambda 4S Long March 1 2A 2E 3 4A Mu 4S 3C 3H 3S 3SII V N1 N-I N-II Naro-1 Paektusan Pilot Proton UR-500 K R-7 Luna Molniya M L Polyot Soyuz original L M U2 Soyuz/Vostok Sputnik Voskhod Vostok L K 2 2M R-29 Shtil' Volna Saturn I IB V INT-21 Scout SLV Space Shuttle Sparta Start-1 Thor Able Ablestar Agena Burner Delta DSV-2U Thorad-Agena Titan II GLV IIIA IIIB IIIC IIID IIIE 34D 23G CT-3 IV Tsyklon 2 3 Vanguard Zenit 2 2M

R-7 rockets

Main articles

Rockets

Missiles

Launch Systems

Sputnik Polyot Voskhod

Vostok	Luna Vostok-L Vostok-K Vostok-2 Vostok-2M

Molniya	Molniya Molniya-M Molniya-L

Soyuz	Soyuz/Vostok Soyuz Soyuz-L Soyuz-M Soyuz-U Soyuz-U2 Soyuz-FG

Soyuz-2	Soyuz 2.1a / STA Soyuz 2.1b / STB Soyuz 2-1v

Launch sites

Baikonur	Site 1/5 Site 31/6

Plesetsk	Site 41/1 Site 16/2 Site 43/3 Site 43/4

Kourou	ELS

Vostochny	Site 1S

Launches

See also

Soyuz human spaceflight programme

Main topics

Current missions

Soyuz MS-02

MS-03

Future missions

2017: Soyuz MS-04; MS-05; MS-06; MS-07
2018: Soyuz MS-08; MS-09; MS-10

Past missions
(by spacecraft type)

Soyuz 7K-OK (1966–1970)	Kosmos 133† Soyuz 7K-OK No.1† Kosmos 140 Soyuz 1† Kosmos 186 188 212 213 238 Soyuz 2 3 4 5 6 7 8 9

Soyuz 7K-L1 (1967–1970) (Zond lunar programme)	Kosmos 146 154† Zond 1967A† 1967B† Zond 4 1968A† 1968B† 5 6 1969A† Zond-M 1† M 2† Zond 7 8 9 10

Soyuz 7K-L1E (1969–1970)	Soyuz 7K-L1E No.1† Kosmos 382

Soyuz 7K-LOK (1971–1972)	Soyuz 7K-LOK No.1† No.2†

Soyuz 7K-OKS (1971)	Soyuz 10† 11†

Soyuz 7K-T (1972–1981)	Kosmos 496 573 Soyuz 12 Kosmos 613 Soyuz 13 Kosmos 656 Soyuz 14 15† 17 18a† 18 20 (uncrewed) 21 23† 24 25† 26 27 28 29 30 31 32 (uncrewed landing) 33† 34 (uncrewed launch) 35 36 37 38 39 40

Soyuz 7K-TM (1974–1976)	Kosmos 638 672 Soyuz 16 19 (Apollo–Soyuz Test Project) 22

Soyuz 7K-S (1974–1976)	Kosmos 670 772† 869†

Soyuz-T (1978–1986)	Kosmos 1001† 1074 Soyuz T-1 (uncrewed) T-2 T-3 T-4 T-5 T-6 T-7 T-8† T-9 T-10a† T-10 T-11 T-12 T-13 T-14 T-15

Soyuz-TM (1986–2002)	Soyuz TM-1 (uncrewed) TM-2 TM-3 TM-4 TM-5 TM-6 TM-7 TM-8 TM-9 TM-10 TM-11 TM-12 TM-13 TM-14 TM-15 TM-16 TM-17 TM-18 TM-19 TM-20 TM-21 TM-22 TM-23 TM-24 TM-25 TM-26 TM-27 TM-28 TM-29 TM-30 TM-31 TM-32 TM-33 TM-34

Soyuz-TMA (2002–2012)	Soyuz TMA-1 TMA-2 TMA-3 TMA-4 TMA-5 TMA-6 TMA-7 TMA-8 TMA-9 TMA-10 TMA-11 TMA-12 TMA-13 TMA-14 TMA-15 TMA-16 TMA-17 TMA-18 TMA-19 TMA-20 TMA-21 TMA-22

Soyuz-TMA-M (2010–2016)	Soyuz TMA-01M TMA-02M TMA-03M TMA-04M TMA-05M TMA-06M TMA-07M TMA-08M TMA-09M TMA-10M TMA-11M TMA-12M TMA-13M TMA-14M TMA-15M TMA-16M TMA-17M TMA-18M TMA-19M TMA-20M

Soyuz MS (2016–present)	Soyuz MS-01

Uncrewed missions are designated with Kosmos numbers; crewed missions get a Soyuz number.
Failed missions are denoted with a † symbol. Cancelled missions are in italics.

This article is issued from Wikipedia - version of the 10/4/2016. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.