| *
Developer:
|
|
* Payload:
| - 7,000 kg |
to ... km Orbit |
|
|
*
Chronology:
| - First Launch Date : |
03/17/1977 |
| - Last Launch Date : |
1981 |
| - Launches |
|
| Total Number: |
47 |
| Number of Failure: |
?? |
| - Success Rate : |
?? % |
|
|
* Launch
Vehicle:
| - Total Mass: |
205,000-210,000 kg |
| - Liftoff Thrust: |
?? kgf |
| - Length with Faring: |
45.66 m |
| - Core Diameter: |
3.09 m |
| - Max. Diameter: |
3.60 m |
|
TSYCLON F1m |
|
* Stage 3:
| - Engine: |
?? |
| - Number of Engines: |
1 |
| - Total Thrust (vac): |
?? kgf |
| - Specific Impulse: |
?? sec |
| - Burn Time: |
?? sec |
| - Gross Mass: |
?? kg |
| - Empty Mass: |
?? kg |
| - Propellants: |
UDMH / RFNA |
| - Length: |
8.93 m |
| - Length Faring: |
8.11 m |
| - Core Diameter: |
2.59 m |
| - max. Diameter Faring: |
2.59 m |
|
|
* Stage 2:
| - Engine: |
RD-252 |
| - Number of Engines: |
2 |
| - Total Thrust (vac): |
97,484 kgf |
| - Specific Impulse: |
318 sec |
| - Burn Time: |
140 sec |
| - Gross Mass: |
48,000 kg |
| - Empty Mass: |
5,000 kg |
| - Propellants: |
UDMH / RFNA |
| - Length: |
9.40 m |
| - Core Diameter: |
3.09 m |
|
|
* Stage 1:
| - Engine: |
RD-251 |
| - Number of Engines: |
6 |
| - Total Thrust (vac): |
279,816 kgf |
| - Burn Time: |
124 sec |
| - Gross Mass: |
125,000 kg |
| - Empty Mass: |
8,500 kg |
| - Propellants: |
UDMH / RFNA |
| - Length: |
18.34 m |
| - Core Diameter: |
3.09 m |
| - max. Diameter: |
3.60 m |
|
|
