* Developer:
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|
* Payload:
8,300 kg |
to 200 km Orbit |
- Payload bay |
2.60 m x 6.80 m |
- Total Habitable Volume: |
46.00 m3 |
|
*
Chronology:
- Start Development : |
ca. 1980 |
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|
* upper
Stage:
- Engine: |
RD-701 |
- Number of Engines: |
2 |
- Total Thrust (vac): |
2 x 2.000 kN |
- Propellants: |
LH2 / LOX /
Kerosene |
|
* Crew:
- crew: |
2 |
- passenger in (pressurized cabin): |
4 |
|
|
*
Spacecraft:
- Total Mass (max): |
27,000 kg |
- Empty Mass: |
18.000 kg |
- Length over all: |
19.30 m |
- max.Hight: |
6.80 m |
- wing Span: |
12.50 m |
- fuselage max. diameter: |
2.60 - 3.00 m |
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