| *
Developer:
|
|
* Payload:
| - 1,400 kg |
to 400 km Orbit |
| - 700 kg |
to 1.600 km Orbit |
|
|
*
Chronology:
| - First Launch Date : |
08/18/1964+?? |
| - Last Launch Date : |
04/24/1996 |
| - Launches |
|
| Total Number: |
415-?? |
| Number of Failure: |
16-?? |
| - Success Rate : |
96.14-?? % |
|
|
* Launch
Vehicle:
| - Total Mass: |
107,500 kg |
| - Liftoff Thrust: |
150,696 kgf |
| - Length with Faring: |
33.05 m |
| - Core Diameter: |
2.40 m |
| - Max. Diameter: |
2.96 m |
|
COSMOS C1 |
|
* Stage 2:
| - Engine: |
RD-?? 11D49 |
| - Number of Engines: |
1 |
| - Total Thrust (vac): |
16,000 kgf |
| - Specific Impulse: |
303 sec |
| - Burn Time: |
375 sec |
| - Gross Mass: |
20,400 kg |
| - Empty Mass: |
1,400 kg |
| - Propellants: |
UDMH / N2 O4 |
| - Length: |
13.40 m |
| - Length Faring: |
5.70 m |
| - Core Diameter: |
2.40 m |
| - max. Diameter: |
3.20 m |
|
|
* Stage 1:
| - Engine: |
RD-216 11D614 |
| - Number of Engines: |
4 |
| - Total Thrust (vac): |
177,433 kgf |
| - Burn Time: |
130 sec |
| - Specific Impulse: |
248 sec |
| - Gross Mass: |
87,100 kg |
| - Empty Mass: |
5,300 kg |
| - Propellants: |
UDMH / N2 O4 |
| - Length: |
19.30 m |
| - Core Diameter: |
2.40 m |
| - max. Diameter: |
2.96 m |
| - Span of Stubilizer: |
4.55 m |
|
|
