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Soyuz · Ministry of Defence of the Russian Federation

Soyuz 2.1b Fregat

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Specifications

Status
active
Height
46.3 m
Diameter
2.95 m
Mass
312,000 kg
Stages
4
Payload to LEO
8,200 kg
Payload to GTO
3,250 kg
First flight
2006-12-27
Total launches
25
Success / Fail
23 / 2

Soyuz-2, GRAU index 14A14, is the collective designation for the 21st-century version of the Russian Soyuz rocket. In its basic form, it is a three-stage carrier rocket for placing payloads into low Earth orbit. The first-stage boosters and two core stages feature uprated engines with improved injection systems, compared to the previous versions of the Soyuz. Digital flight control and telemetry systems allow the rocket to be launched from a fixed launch platform, whereas the launch platforms for earlier Soyuz rockets had to be rotated as the rocket could not perform a roll to change its heading in flight. The Soyuz 2.1b represents the latest development stage of the proven rocket. It uses the new RD-0124 engines in the first three stages, coupled with an improved injection system that significantly boosts the performance of the Soyuz. Furthermore, she wears a new, digital startup control system. This will allow the Soyuz 2.1b to carry around 1.2 tonnes more payload into low earth orbit compared to its predecessor.

Payloads it launched · 65

COSMOS 2596 [GLONASS-K1]
MEO
COSMOS 2595 (MOZHAETS 6)
MEO
COSMOS 2563
HEO
COSMOS 2559 [GLONASS-K]
MEO
COSMOS 2557 [GLONASS-K]
MEO
COSMOS 2552
GEO
COSMOS 2547 [GLONASS-K]
MEO
COSMOS 2546
HEO
COSMOS 2541
GEO
ICEYE-X4
LEO
LEMUR-2-EJATTA
LEO
OBJECT B
LEO
DOT-1
LEO
ROBUSTA-1C (MTCUBE 1)
LEO
LEMUR-2-GREGROBINSON
LEO
D-STAR ONE (EXOCONNECT)
LEO
MOMENTUS-X1
LEO
SONATE
LEO
LEMUR-2-ALEX-MADDY
LEO
VDNH-80
LEO
METEOR-M2 2
LEO
LEMUR-2-DUSTINTHEWIND
LEO
MOVE-IIB
LEO
SOKRAT
LEO