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Soyuz 2.1a
PRSC
Details
Height
46.3 m
Diameter
2.95 m
GTO
2,810 kg
LEO
7,020 kg
Thrust at Liftoff
4,149 kN
Apogee
Unknown
Launch Cost
$80M
Maiden Flight
November 4, 2004
Statistics
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Description
The Soyuz 2.1A converted the flight control system from analog to digital, which allowed launch from fixed platforms. It also allowed big fairings and payloads. It is currently used for crewed Soyuz and Progress flights to the ISS.
Agency
Progress Rocket Space Center
PRSC
Links
Wikipedia
en.wikipedia.org