| *
Developer:
|
|
* Payload:
| - (3,600) kg |
to 200 km Orbit |
|
|
*
Chronology:
| - First Launch Date : |
(101/24/1969) |
| - Last Launch Date : |
(02/19/1996) |
| - Launches |
|
| Total Number: |
(119) |
| Number of Failure: |
(7) |
| - Success Rate : |
(94,12 %) |
|
|
* Launch
Vehicle:
| - Total Mass: |
(184,900)
kg |
| - Empty Mass: |
?? kg |
| - Liftoff Thrust: |
(280,132) kgf |
| - Length without Faring: |
(31.6)
m |
| - Core Diameter: |
3.09 m |
| - Max. Diameter: |
3.60 m |
|
TSYCLON 3 |
|
* Stage 3:
| - Engine: |
?? (RD-?? 11D25) |
| - Number of Engines: |
1 |
| - Total Thrust (vac): |
(8,117) kgf |
| - Specific Impulse: |
(317) sec |
| - Burn Time: |
(125) sec |
| - Gross Mass: |
(4,600) kg |
| - Empty Mass: |
(1,600) kg |
| - Propellants: |
UDMH / N2 O4 |
| - Length: |
(2,80) m |
| - Length Faring: |
7.68 m |
| - Core Diameter: |
(2.20) m |
| - Core Diameter Faring: |
2.80 m |
|
|
* Stage 2:
| - Engine: |
RD-(252) |
| - Number of Engines: |
2 |
| - Total Thrust (vac): |
(102,993) kgf |
| - Specific Impulse: |
(318) sec |
| - Burn Time: |
160 sec (140) |
| - Main Engine Burn Time: |
160 sec |
| - Conttrol Engine Burn Time: |
163 sec |
| - Gross Mass: |
(53,300) kg |
| - Empty Mass: |
(4,800) kg |
| - Propellants: |
UDMH / N2 O4 |
| - Length: |
(10.10) m |
| - Core Diameter: |
3.09 m |
|
|
* Stage 1:
| - Engine: |
RD-(251) |
| - Number of Engines: |
6 |
| - Total Thrust (at the sea level): |
(309,183 ) kgf |
| - Burn Time: |
(298) sec |
| - Main Engine Burn Time: |
(120) sec |
| - Conttrol Engine Burn Time: |
?? sec |
| - Gross Mass: |
(127,000) kg |
| - Empty Mass: |
(8,300) kg |
| - Propellants: |
UDMH / N2 O4 |
| - Length: |
(18.80) m |
| - Core Diameter: |
3.09 m |
| - max. Diameter: |
3.60 m |
|
|
