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Soyuz-2

Soyuz-2

Space Launch Systems
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Basic Information
Name
Soyuz-2
Designation
Soyuz-2
Alternate Designation
R-7A, Soyuz-2.1b, Soyuz-2.1V (December 2013), Soyuz-2-1A, Soyuz-2-1B, Soyuz-ST
Equipment Type
Space Launch Systems
Manufacturer
Starsem, TsSKB Progress
Date of Introduction
2006
Description

The Soyuz-2 is a further development to extend the service life of launch vehicle Soyuz well into the second the decade of the 21st century. The Soyuz-2 features greater payload, improved injection into orbit accuracy and eliminates the usage of high-toxic fuel components. The Soyuz-2 development was split between Soyuz-2-1A and Soyuz-2-1B phases. The first Soyuz-2-1A was launched November 2004 carrying a test payload and put into orbit the MetOp-A meteorological satellite in October 2006. The first Soyuz-2-1B was launched December 2006 carrying Corot scientific spacecraft. The Soyuz-ST is a version designed for launch from the Kourou space center in the French Guiana. The Soyuz-2 has been designed as the replacement for current Soyuz-series and Molniya-M space launch vehicles. The upgraded Soyuz-ST launch vehicle introduces an increased payload volume and weight to meet the increasing needs of international customers as well as a new digital flight control system to improve trajectory accuracy. Some parts of Soyuz/ST propulsion system have been reinforced and propellant tanks have been enlarged. The Soyuz-ST launch vehicle will carry a 10,800 lb (4,900 kg) payload to a Low Earth Orbit (LEO). Using Fregat upper stage, Soyuz-ST will deliver a 12,125 lb (5,500 kg) payload to LEO and a 10,141 lb (4,600 kg) to a Sun Synchronous Orbit (SSO). The Soyuz-2.1V is a new light rocket launcher equipped with a powerful NK-33-1 engine and capable of delivering a payload of 2.8 tons into a Low Earth Orbit. The first launch of a Soyuz-2.1V rocket launch system was scheduled for early 2013 but finally was carried out on December 28, 2013. The Soyuz-2.1b performed its final launch from Plesetsk cosmodrome on February 5, 2025. The Soyuz-2.1a will remain active launching Soyuz Progress spacecraft.

Overview (Deagel)
Group Space Launch Systems
Status Active
Also Known As R-7A, Soyuz-2.1b, Soyuz-2.1V (December 2013), Soyuz-2-1A, Soyuz-2-1B, Soyuz-ST
Origin Russia
Contractors Starsem, TsSKB Progress
Initial Operational Capability (IOC) October 19, 2006
First Flight November 8, 2004
Total Production 175
Unitary Cost USD $40 million
Specifications (Deagel)
Crew 0
Number of Stages 3
Dimensions — Height 49 meter
Dimensions — Rocket Diameter 2.7 meter
Mass — Max Lift-off Thrust 910,000 pound
Mass — Max Lift-off Weight 290 ton
Mass — Payload to LEO 5,500 kilogram
Mass — Payload to SSO 4,600 kilogram
Gear (Deagel)
Item 1 Satellites: GLONASS-K (1)
Item 2 Satellites: GLONASS-M (1)
Item 3 Spaceships: Soyuz TMA (1)
Variants
Variant 1 Molniya-M
Variant 2 Soyuz-U
Variant 3 Soyuz-Ikar
Variant 4 Soyuz-Fregat
Variant 5 Soyuz-2
Details
Country of Origin Russia
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
49 m
Width
2.7 m
Height
49 m
Weight
290000 kg
Operators (1)
Russia
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