| *
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 |
|
|
