* Developer:
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* Payload:
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*
Chronology:
- First Launch Date : |
09/17/1966 |
- Last Launch Date : |
08/09/1971 |
- Launches |
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Total Number: |
18 |
Number of Failure: |
0 |
- Success Rate : |
100 % |
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* Launch
Vehicle:
- Total Mass: |
173,000 kg |
- Liftoff Thrust: |
253,524 kgf |
- Length with Faring: |
36.36 m |
- Core Diameter: |
3.09 m |
- Max. Diameter: |
3.60 m |
|
TSYCLON F1r |
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* Stage 2:
- Engine: |
RD-252 |
- Number of Engines: |
2 |
- Total Thrust (vac): |
97,484 kgf |
- Specific Impulse: |
318 sec |
- Burn Time: |
140 sec |
- Gross Mass: |
48,000 kg |
- Empty Mass: |
5,000 kg |
- Propellants: |
UDMH / RFNA |
- Length: |
9.40 m |
- Length Faring: |
7.76 m |
- Core Diameter: |
3.09 m |
- max. Diameter Faring: |
2.33 m |
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* Stage 1:
- Engine: |
RD-251 |
- Number of Engines: |
6 |
- Total Thrust (vac): |
279,816 kgf |
- Burn Time: |
124 sec |
- Gross Mass: |
125,000 kg |
- Empty Mass: |
8,500 kg |
- Propellants: |
UDMH / RFNA |
- Length: |
18.34 m |
- Core Diameter: |
3.09 m |
- max. Diameter: |
3.60 m |
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