| * Developer:
|
|
* Payload:
| - 2,900 kg (2.800) |
to 200 km Orbit |
|
|
*
Chronology:
| - First Launch Date : |
August 1969 (10/27/1967) |
| - Last Launch Date : |
in service
(12/20/1995) |
| - Launches |
|
| Total Number: |
101 (due July 1-st, 1997)
(102) |
| Number of Failure: |
0(1) |
| - Success Rate : |
100 % (99,02
%) |
|
|
* Launch
Vehicle:
| - Total Mass: |
176,000 kg |
| - Empty Mass: |
11,600 kg |
| - Liftoff Thrust: |
2,364 kN
(253,524 kgf=2486 kN) |
| - Length without Faring: |
28.30 m
(30.9) |
| - Core Diameter: |
3.09 m |
| - Max. Diameter: |
3.60 m |
|
TSYCLON 2M |
|
* Stage 3:
| - Engine: |
?? (RD-?? 11D25) |
| - Number of Engines: |
1 |
| - Total Thrust (vac): |
(7,950) kgf |
| - Specific Impulse: |
(317) sec |
| - Burn Time: |
(112) sec |
| - Gross Mass: |
(3,200) kg |
| - Empty Mass: |
(400) kg |
| - Propellants: |
UDMH / N2 O4 |
| - Length: |
(4.00) m |
| - Length Faring: |
10.50 m |
| - Core Diameter: |
(2.00) m |
| - max. Diameter Faring: |
2.80 m |
|
|
* Stage 2:
| - Engine: |
RD-262 (252) |
| - Number of Engines: |
2 |
| - Total Thrust (vac): |
941 kN (97,484 kgf=956 kN) |
| - Specific Impulse: |
(318) sec |
| - Burn Time: |
160 sec (140) |
| - Gross Mass: |
48,000 kg |
| - Empty Mass: |
5,000 kg |
| - Propellants: |
UDMH / N2 O4 |
| - Length: |
9.40 m (8.30) |
| - Core Diameter: |
3.09 m |
|
|
* Stage 1:
| - Engine: |
RD-261 (251) |
| - Number of Engines: |
6 |
| - Total Thrust (at the sea level): |
2364 kN (309,183 kgf) |
| - Burn Time: |
(298) sec |
| - Main Engine Burn Time: |
120 sec |
| - Conttrol Engine Burn Time: |
125 sec |
| - Gross Mass: |
125,000 kg (127,000) |
| - Empty Mass: |
8,500 kg (8,300) |
| - Propellants: |
UDMH / N2 O4 |
| - Length: |
18.90 m (18.80) |
| - Core Diameter: |
3.09 m |
| - max. Diameter: |
3.60 m |
|
|
