| *
Developer:
|
* Payload:
| - 1,400 kg |
to 220 km Orbit |
|
|
*
Chronology:
| - First Launch Date : |
07/04/1983 |
| - Last Launch Date : |
08/27/1987 |
| - Launches |
|
| Total Number: |
5 |
| Number of Failure: |
0 |
| - Success Rate : |
100 % |
|
* Launch
Vehicle:
| - Total Mass: |
107,500 kg |
| - Liftoff Thrust: |
150,696 kgf |
| - Length with Faring: |
35.47 m |
| - Core Diameter: |
3.90 m |
|
COSMOS BOR 5 |
*
Spacecraft: 1/8 scale model of BURAN
| - Total Mass: |
1,400 kg |
| - Length over all: |
4.50 m |
| - Wing Span: |
3.00 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 |
|
|
