| *
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 VOSTOCK |
* VOSTOCK:
| - Total Mass: |
4,730 kg |
| - Length over all: |
4.40 m |
| - Fuselage Diameter: |
2.40 m |
|
 |
* Stage 2:
(Vostock 2)
| - Engine: |
RD-0109 |
| - Number of Engines: |
1 |
| - Total Thrust (vac): |
5,600 kgf |
| - Specific Impulse: |
326 sec |
| - Burn Time: |
369 sec |
| - Gross Mass: |
7,775 kg |
| - Empty Mass: |
1,440 kg |
| - Propellants: |
Kerosene / LOX |
| - Length: |
2.80 m |
| - Core Diameter: |
2.80 m |
|
* Stage 1:
(Vostock-1)
| - Engine: |
8D75K |
| - Number of Engines: |
4 |
| - Total Thrust (vac): |
95,900 kgf |
| - Specific Impulse: |
315 sec |
| - Burn Time: |
301 sec |
| - Gross Mass: |
100,400 kg |
| - Empty Mass: |
6,800 kg |
| - Propellants: |
Kerosene / LOX |
| - Length: |
28,00 m |
| - Core Diameter (conical): |
3,00 m |
|
|
* Stage 0:
(Vostock-0)
| - Engine: |
8D74K |
| - Number of Engines: |
4 |
| - Total Thrust (vac): |
101,500 kgf |
| - Burn Time: |
118sec |
| - Specific Impulse: |
313 sec |
| - Gross Mass: |
43,300 kg |
| - Empty Mass: |
3,710 kg |
| - Propellants: |
Kerosene / LOX |
| - Length: |
19.00 m |
| - Core Diameter: |
2.70 m |
| - max. Diameter: |
3.00 m |
|
|
