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COSMOS-BOR 4 launch vehicle


COSMOS - BOR 4
US DoD: SL-?

* Developer:
NPO Yuzhnoye (Ukraine)
* Payload:
- 1,000 kg to 220 km Orbit
* Chronology:
- First Launch Date : 06/04/1982
- Last Launch Date : 12/19/1984
- Launches
    Total Number: 4
    Number of Failure: 0
- Success Rate : 100 %
* Launch Vehicle:
- Total Mass: 107,500 kg
- Liftoff Thrust: 150,696 kgf
- Length with Faring: 35.36 m
- Core Diameter: 3.90 m

Cosmos-BOR-4

COSMOS BOR 4

* Spacecraft: scale model of URAGAN
- Total Mass:

1,000 kg

- Length over all: 7.46 m
- Wing Span: 5.35 m
- Fuselage Diameter: 0.70 m

Space plane BOR-4

* solid rocket motors block:
- Engine: ??
- Number of Engines: 12
- Total Thrust (vac): ?? kgf
- Propellants: ??
- Length: 1.74 m
- Core Diameter (conical): 2.44 m
* 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 Payload

* 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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