Soyuz (rocket)

Soyuz 11A511

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
Size
Height	45.6 metres (150 ft)
Diameter	10.3 metres (34 ft)
Mass	308,000 kilograms (679,000 lb)
Stages	3
Capacity
Payload to LEO
Mass	6,450 kilograms (14,220 lb)
Associated rockets
Family	R-7 (Soyuz)
Derivative work	Soyuz-L Soyuz-M Soyuz-U
Launch history
Status	Retired
Launch sites	Baikonur Sites 1/5 & 31/6
Total launches	32[1]
Success(es)	30
Failure(s)	2
First flight	28 November 1966
Last flight	14 October 1976
Type of passengers/cargo	Soyuz
Boosters – Block A/B/V/G
No. boosters	4
Powered by	1 RD-107
Maximum thrust	994.3 kilonewtons (223,500 lbf)
Specific impulse	315 sec
Burn time	118 seconds
Propellant	RP-1/LOX
First stage – 11S59
Powered by	1 RD-108
Maximum thrust	977.7 kilonewtons (219,800 lbf)
Specific impulse	315 sec
Burn time	292 seconds
Propellant	RP-1/LOX
Second stage – 11S510
Powered by	1 RD-0110
Maximum thrust	294 kilonewtons (66,000 lbf)
Specific impulse	330 sec
Burn time	246 seconds
Propellant	RP-1/LOX
[edit on Wikidata]

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 uncrewed test flights, followed by the first 19 crewed 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 and was an attempt to standardize the R-7 family and get rid of the variety of models that existed up to that point. It was basically a Molniya 8K78M sans the Blok L stage and featured the 8D74M RD-107 and the RD-110 engines from the 8K78M,^[2] 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. The RD-0110 engine had been introduced on the 8K78M booster in 1964 and was also used in 11A511s due to its enhanced performance while Voskhod boosters continued using the less powerful RD-0107.^[3]

The AVD malfunction detection system, variants of which are a standard component of all Soviet/Russian SLVs, would issue an automatic shutdown command to the booster in the event that operating parameters such as electrical power, engine performance, or flight trajectory deviated from normal, and on manned launches also activate the Launch Escape System. This would prevent a malfunctioning launch vehicle from flying around erratically and ensure it fell to the ground and impacted in a predictable location. The AVD on the 11A511 was blocked from operating until T+8 seconds to ensure the booster's systems had stabilized and entered mainstage operation, but the actual shutdown command was not transmitted until T+20 seconds to prevent the booster from falling back on the pad. Nonetheless, several launches failed over the years due to problems with the AVD itself issuing erroneous shutdown commands.

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 crewed 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.^[4]