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TSYCLON-F1r launch vehicle

TSYCLON-F1r
US DoD: SL-?

* Developer:
M.Yangel Design Bureau
* Payload:
- 500 kg to 150 km

Payload
* Chronology:
- First Launch Date : 09/17/1966
- Last Launch Date : 08/09/1971
- Launches
    Total Number: 18
    Number of Failure: 0
- Success Rate : 100 %
* 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

TSYCLON F1r

 * 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

Stage 2 without Payload
* 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

Stage 1

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