| *
Developer:
|
|
* Payload:
| - 13,740 kg |
to 200 km Orbit |
| - 5,180 kg |
to Geosynchronous transfer trajectory |
|
|
*
Chronology:
| - First Launch Date : |
1998 |
| - Last Launch Date : |
in service |
| - Launches |
|
| Total Number: |
0 |
| Number of Failure: |
0 |
| - Success Rate : |
% |
|
|
* Launch
Vehicle:
| - Total Mass: |
461,900 kg |
| - Liftoff Thrust: |
769,880 kgf |
| - Length with Faring: |
49.90 m |
| - Core Diameter: |
3.90 m |
|
ZENIT 3 sea launch |
|
* Block
DM-SL:
| - Engine: |
RD-58 11D58D |
| - Number of Engines: |
1 |
| - Total Thrust (vac): |
7,240 kgf |
| - Specific Impulse: |
361 sec |
| - Burn Time: |
660 sec |
| - Gross Mass: |
17,300 kg |
| - Empty Mass: |
3,100 kg |
| - Propellants: |
Kerosene / LOX |
| - Length: |
5.50 m |
| - Length Faring: |
8.54 m |
| - Core Diameter: |
3.74 m |
|
|
* Stage 2:
| - Engine: |
RD-120 11D123 |
| - Number of Engines: |
1 |
| - Total Thrust (vac): |
93,000 kgf |
| - Specific Impulse: |
349+?? sec |
| - Burn Time: |
315+?? sec |
| - Gross Mass: |
90,400+?? kg |
| - Empty Mass: |
8,400+?? kg |
| - Propellants: |
Kerosene / LOX |
| - Length: |
15.90 m |
| - Core Diameter: |
3.90 m |
|
|
* Stage 1:
| - Engine: |
RD-171 11D520 |
| - Number of Engines: |
4 |
| - Total Thrust (vac): |
834,243 kgf |
| - Specific Impulse: |
337 sec |
| - Burn Time: |
150 sec |
| - Gross Mass: |
354,200 kg |
| - Empty Mass: |
27,900 kg |
| - Propellants: |
Kerosene / LOX |
| - Length: |
32.06 m |
| - Core Diameter: |
3.90 m |
|
|
