| *
Developer:
|
|
* Payload:
| - 1.000 kg |
to 220 km Orbit |
|
|
*
Chronology:
| - First Launch Date : |
08/01/1987 |
| - Last Launch Date : |
08/28/1987 |
| - Launches |
|
| Total Number: |
2 |
| Number of Failure: |
0 |
| - Success Rate : |
100 % |
|
|
* Launch
Vehicle:
| - Total Mass: |
461.900 kg |
| - Liftoff Thrust: |
769,880 kgf |
| - Length with Faring: |
56.00 m |
| - Core Diameter: |
3.90 m |
|
ZENIT URAGAN |
|
*
Spacecraft: 1/3 scale model of URAGAN
| - Total Mass: |
1,400 kg |
| - Length over all: |
4.50 m |
| - Wing Span: |
3.00 m |
| - Fuselage Diameter: |
0.70 m |
|
|
* solid
rocket motors block:
| - Engine: |
?? |
| - Number of Engines: |
12 |
| - Total Thrust (vac): |
?? kgf |
| - Propellants: |
?? |
| - Length: |
1.74 m |
| - Core Diameter (conical): |
2.44 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: |
11.50 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 |
|
|
