*
Developer:
|
|
* Payload:
- more than 100,000 kg |
to LEO |
- 22,000 kg |
Geosynchronous Orbit |
|
|
*
Chronology:
- First Launch Date : |
05/15/1987 |
- Last Launch Date : |
11/15/1988 |
- Launches |
|
Total Number: |
2 |
Number of Failure: |
0 |
- Success Rate : |
100 % |
|
|
* Launch
Vehicle:
- Total Mass: |
2,419,000 kg |
- Empty Mass: |
about 300,000 kg |
- Liftoff Thrust: |
3,582,253 kgf |
- Total Length: |
58,76 m |
- Core Diameter: |
7,75 m |
|
ENERGIYA |
|
* Stage 2:
(Energiya RCS Retro & Correction Stage)
- Engine: |
RD-58 11D58D |
- Number of Engines: |
1 |
- Total Thrust (vac): |
8,661 kgf |
- Specific Impulse: |
352 sec |
- Burn Time: |
680 sec |
- Control Engine Burn Time: |
0 sec |
- Gross Mass: |
17,000 kg |
- Empty Mass: |
2,000 kg |
- Propellants: |
Kerosene / LOX |
- Length: |
5.70 m |
- Core Diameter: |
3.70 m |
|
|
* Stage 1:
(Energiya Core)
- Engine: |
RD-01200 11D122 RO-200 |
- Number of Engines: |
4 |
- Total Thrust (vac): |
800,286 kgf |
- Specific Impulse: |
453 sec |
- Burn Time: |
480 sec |
- Control Engine Burn Time: |
354 sec |
- Gross Mass: |
905,000 kg |
- Empty Mass: |
85,000 kg |
- Propellants: |
LH2 / LOX |
- Length: |
58.76 m |
- Core Diameter: |
7.80 m |
|
* Stage 0:
(4 x Energiya Strapon)
- Engine: |
RD-170 11D251 |
- Number of Engines: |
4 x 4 |
- Total Thrust (vac): |
4 x 806,400 kgf |
- Burn Time: |
145 sec |
- Specific Impulse: |
337 sec |
- Control Engine Burn Time: |
309 sec |
- Gross Mass: |
4 x 355,000 kg |
- Empty Mass: |
4 x 35,000 kg |
- Propellants: |
Kerosene / LOX |
- Length: |
36.46 m |
- Core Diameter: |
3.90 m |
- max.Span: |
4.20 m |
|
|