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Launch Vehicle

Soyuz-U2

retired
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Specifications

Status
retired
Height
34.54 m
Diameter
2.95 m
Mass
298,000 kg
Stages
2
Thrust
4,144 kN
Payload to LEO
7,050 kg
First flight
1982-12-23
Total launches
71
Success / Fail
71 / 0

The Soyuz-U2 was a Soviet, later Russian, carrier rocket. It was derived from the Soyuz-U, and a member of the R-7 family of rockets. It featured increased performance compared with the baseline Soyuz-U, due to the use of syntin propellant, as opposed to RP-1 paraffin, used on the Soyuz-U.

Propulsion

Boosters

4×RD-107A838 kN
RP-1 / LOX · gas-generator
NPO Energomash / KuznetsovIsp 320s (vac)since 2004four boosters

First stage

RD-108A792 kN
RP-1 / LOX · gas-generator
NPO Energomash / KuznetsovIsp 315s (vac)since 2001core

Third stage

RD-0110298 kN
RP-1 / LOX · gas-generator
KBKhAIsp 326s (vac)since 1967Blok I

Payloads it launched

60 loaded
SOYUZ-TM 22
LEO
SOYUZ-TM 21
LEO
SOYUZ-TM 20
LEO
SOYUZ-TM 19
LEO
SOYUZ-TM 18
LEO
COSMOS 2262
LEO
SOYUZ-TM 17
LEO
PROGRESS-M 18
LEO
PROGRESS-M 17
LEO
PROGRESS-M 16
LEO
SOYUZ-TM 16
LEO
PROGRESS-M 15
LEO
PROGRESS-M 14
LEO
SOYUZ-TM 15
LEO
PROGRESS-M 13
LEO
PROGRESS-M 12
LEO
SOYUZ-TM 14
LEO
PROGRESS-M 11
LEO
PROGRESS-M 10
LEO
COSMOS 2163
LEO
SOYUZ-TM 13
LEO
PROGRESS-M 9
LEO
PROGRESS-M 8
LEO
SOYUZ-TM 12
LEO
PROGRESS-M 7
LEO
PROGRESS-M 6
LEO
SOYUZ-TM 11
LEO
COSMOS 2101
LEO
PROGRESS-M 5
LEO
PROGRESS-M 4
LEO
SOYUZ-TM 10
LEO
GAMMA
LEO
PROGRESS 42
LEO
PROGRESS-M 3
LEO
SOYUZ-TM 9
LEO
PROGRESS-M 2
LEO
SOYUZ-TM 8
LEO
PROGRESS-M 1
LEO
PROGRESS 41
LEO
PROGRESS 40
LEO
PROGRESS 39
LEO
SOYUZ-TM 7
LEO
PROGRESS 38
LEO
SOYUZ-TM 6
LEO
PROGRESS 37
LEO
SOYUZ-TM 5
LEO
SOYUZ-TM 5 ORBIT MODULE
LEO
PROGRESS 36
LEO
PROGRESS 35
LEO
PROGRESS 34
LEO
SOYUZ-TM 4 ORBIT MODULE
LEO
SOYUZ-TM 4
LEO
PROGRESS 33
LEO
PROGRESS 32
LEO
PROGRESS 31
LEO
SOYUZ-TM 3
LEO
SOYUZ-TM 3 ORBIT MODULE
LEO
PROGRESS 30
LEO
PROGRESS 29
LEO
PROGRESS 28
LEO