*
Developer:
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* Payload:
- 1,000 kg |
to 220 km Orbit |
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*
Chronology:
- First Launch Date : |
06/04/1982 |
- Last Launch Date : |
12/19/1984 |
- Launches |
|
Total Number: |
4 |
Number of Failure: |
0 |
- Success Rate : |
100 % |
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|
* 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 |
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*
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 |
|
|
* 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 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 |
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