*
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 |
|
INTERCOSMOS |
|
* 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: |
13.05 m |
- Length Faring: |
6.05 m |
- Core Diameter: |
2.40 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 |
|
|