| * Developer:
|
|
* Payload:
|
|
*
Chronology:
| - First Launch Date : |
09/23/1968 |
| - Last Launch Date : |
08/29/1991 |
| - Launches |
|
| Total Number: |
153 |
| Number of Failure: |
15 |
| - Success Rate : |
90.2 % |
|
|
* Launch
Vehicle:
| - Total Mass: |
281,375 kg |
| - Liftoff Thrust: |
407,565 kgf |
| - Length with Faring: |
30.80 m |
| - Core Diameter: |
3.00 m |
|
R-7 SOJUS |
|
* SOJUS:
| - Total Mass: |
7.070 kg |
| - Length over all: |
6.98 m |
| - Fuselage Diameter: |
2.40 m |
|
 |
* Stage 2:
(Soyus 2)
| - Engine: |
11D5 |
| - Number of Engines: |
4 |
| - Total Thrust (vac): |
30,408 kgf |
| - Specific Impulse: |
330 sec |
| - Burn Time: |
250 sec |
| - Gross Mass: |
25,400 kg |
| - Empty Mass: |
2,400 kg |
| - Propellants: |
Kerosene / LOX |
| - Length: |
6.70 m |
| - Core Diameter: |
2.70 m |
|
* Stage 1:
(Soyus-1)
| - Engine: |
11D512 |
| - Number of Engines: |
4 |
| - Total Thrust (vac): |
101,633 kgf |
| - Specific Impulse: |
315 sec |
| - Burn Time: |
250 sec |
| - Gross Mass: |
101,000 kg |
| - Empty Mass: |
6,500 kg |
| - Propellants: |
Kerosene / LOX |
| - Length: |
27.800 m |
| - Core Diameter (conical): |
3,00 m |
|
|
* Stage 0:
(Soyus-0)
| - Engine: |
11D511 |
| - Number of Engines: |
4 |
| - Total Thrust (vac): |
101,134 kgf |
| - Burn Time: |
11 sec |
| - Specific Impulse: |
314 sec |
| - Gross Mass: |
42,750 kg |
| - Empty Mass: |
3,550 kg |
| - Propellants: |
Kerosene / LOX |
| - Length: |
19.60 m |
| - Core Diameter: |
2.70 m |
| - max. Diameter: |
3.00 m |
|
|
