| * Developer:
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* Payload:
|
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*
Chronology:
| - First Launch Date : |
03/16/1962 (10/26/1961
2 times Failures) |
| - Last Launch Date : |
06/18/1977 |
| - Launches |
|
| Total Number: |
148 |
| Number of Failure: |
2 |
| - Success Rate : |
98.65 % |
|
|
* Launch
Vehicle:
| - Total Mass: |
48,110 kg |
| - Liftoff Thrust: |
64,905 kgf |
| - Length with Faring: |
28.42 m |
| - Core Diameter: |
1.65 m |
| - Max. Diameter: |
2.30 m |
|
COSMOS B1 |
|
* Stage 2:
| - Engine: |
RD-119 8D710 |
| - Number of Engines: |
1 |
| - Total Thrust (vac): |
10,760 kgf |
| - Specific Impulse: |
352 sec |
| - Burn Time: |
250 sec |
| - Gross Mass: |
8,595 kg |
| - Empty Mass: |
840 kg |
| - Propellants: |
UDMH / LOX |
| - Length: |
7.80 m |
| - Length Faring: |
2.62 m |
| - Core Diameter: |
1.65 m |
|
|
* Stage 1:
| - Engine: |
RD-214 |
| - Number of Engines: |
4 |
| - Total Thrust (vac): |
74,500 kgf |
| - Burn Time: |
125 sec |
| - Specific Impulse: |
352 sec |
| - Gross Mass: |
39,515 kg |
| - Empty Mass: |
3,150 kg |
| - Propellants: |
Kerosene / RFNA |
| - Length: |
19.30 m |
| - Core Diameter: |
1.65 m |
| - max. Diameter: |
2.30 m |
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