| *
Developer:
|
|
* Payload:
| - 1,400 kg |
to 400 km Orbit |
| - 700 kg |
to 1.600 km Orbit |
|
|
*
Chronology:
| - First Launch Date : |
02/21/1969 |
| - Last Launch Date : |
11/23/1972 |
| - Launches |
|
| Total Number: |
4 |
| Number of Failure: |
4 |
| - Success Rate : |
0 % |
|
|
* Launch
Vehicle:
| - Total Mass: |
2,682,650 kg |
| - Liftoff Thrust: |
4,414,909 kgf |
| - Length with Faring: |
105.00 m |
| - Core Diameter(conical): |
16.88 m |
| - Max. Diameter: |
22.33 m |
|
N1-L3
|
|
* Stage 5:
(Block D)
| - Engine: |
RD-58 1D58D |
| - Number of Engines: |
1 |
| - Total Thrust (vac): |
8,700 kgf |
| - Specific Impulse: |
348 sec |
| - Burn Time: |
600 sec |
| - Gross Mass: |
17,650 kg |
| - Empty Mass: |
2,650 kg |
| - Propellants: |
Kerosene / LOX |
| - Length: |
5.70 m |
| - Core Diameter: |
2.90 m |
|
|
*Stage 4: (Block G)
| - Engine: |
NK-19 11D54 |
| - Number of Engines: |
1 |
| - Total Thrust (vac): |
45,479 kgf |
| - Specific Impulse: |
353 sec |
| - Burn Time: |
443 sec |
| - Gross Mass: |
65,000 kg |
| - Empty Mass: |
7,000 kg |
| - Propellants: |
Kerosene / LOX |
| - Length: |
8.90 m |
| - Core Diameter: |
4.40 m |
|
|
*Stage 3:
(Block V)
| - Engine: |
NK-19 11D53 |
| - Number of Engines: |
4 |
| - Total Thrust (vac): |
164,000 kgf |
| - Specific Impulse: |
353 sec |
| - Burn Time: |
370 sec |
| - Gross Mass: |
185,000 kg |
| - Empty Mass: |
10,000 kg |
| - Propellants: |
Kerosene / LOX |
| - Length: |
12.00 m |
| - Core Diameter: |
4.80 m |
| - max. Diameter: |
7.59 m |
| - Span of Stubilizer: |
6.80 m |
|
|
* Stage 2:
(Block B)
| - Engine: |
NK-19 11D52 |
| - Number of Engines: |
8 |
| - Total Thrust (vac): |
1,431,680 kgf |
| - Specific Impulse: |
346 sec |
| - Burn Time: |
120 sec |
| - Gross Mass: |
540,000 kg |
| - Empty Mass: |
35,000 kg |
| - Propellants: |
Kerosene / LOX |
| - Length: |
20.00 m |
| - Core Diameter: |
6.80 m |
| - max. Diameter: |
10.30 m |
| - Span of Stubilizer: |
9.80 m |
|
|
* Stage 1:
(Block A)
| - Engine: |
NK-19 11D51 |
| - Number of Engines: |
30 |
| - Total Thrust (vac): |
5,130,000 kgf |
| - Specific Impulse: |
330 sec |
| - Burn Time: |
125 sec |
| - Gross Mass: |
1,875,000 kg |
| - Empty Mass: |
125,000 kg |
| - Propellants: |
Kerosene / LOX |
| - Length: |
30.00 m |
| - Core Diameter: |
10.00 m |
| - max. Diameter: |
16.88 m |
| - Span of Stubilizer: |
22.33 m |
|
