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INTERCOSMOS launch vehicle


INTERCOSMOS
US DoD:  SL-?

* Developer:
M.Yangel Design Bureau
* Payload:
- 1,400 kg to 400 km Orbit
- 700-?? kg to 1.600 km Orbit

Payload

* 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

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 2 without Faring

* 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

Stage 1

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COSMOS launch vehicles
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