Soyuz-Fregat
Soyuz-Fregat
Space Launch Systems
Basic Information
Name
Soyuz-Fregat
Designation
Soyuz-Fregat
Alternate Designation
R-7, Soyuz-FG
Equipment Type
Space Launch Systems
Manufacturer
Starsem
Date of Introduction
2000
Description
The Soyuz-Fregat launch system includes the Fregat upper stage with more propellant charge and a restart capability as many as 20 times. It can perform a full range of missions ranging from put into orbit missions to Earth escape missions in support of outer space exploration spacecrafts (Mars Express). The Soyuz-Fregat launch vehicle can deliver payloads of 11,022 lb (5,000 kg) to LEO (450 km altitude), or 8,818 lb (4,000 kg) to a Sun Synchronous Orbit (SSO 1,400 km altitude). The Soyuz-Fregat was retired in 2013.
Overview (Deagel)
Group
Space Launch Systems
Status
Retired - No Longer Operational
Also Known As
R-7, Soyuz-FG
Origin
Russia
Contractor
Starsem
Initial Operational Capability (IOC)
2000
Total Production
23
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
5,000 kilogram
Mass — Payload to SSO
4,000 kilogram
Gear (Deagel)
Item 1
Satellites: MetOp (1)
Item 2
Spaceships: Soyuz TMA-M (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
Sources
deagel.com: https://www.deagel.com/x/x/a000231
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
—
Width
2.7 m
Height
49 m
Weight
290000 kg
Operators (1)
Russia
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