| Characteristic |
Variants |
|
Basic |
Intermediate |
| GSR's fuel |
Liquide hydrogen |
Kerozen |
| Auxiliary rocket's fuel |
Liquid fluor + Liquid hydrogen |
Liquid oxygen + Liquid hydrogen |
| OS's fuel |
F2 + NH3 |
AT + UDMH |
| Lift off mass, kg |
115000 |
129920 |
| GSR's characteristics |
|
|
| Lift off mass, kg |
52000 |
72000 |
| Empty mass, kg |
36000 |
38400 |
| Velocity, m/s |
1800 (M=6) |
1200 (M=4) |
| Ceiling, km |
28-30 |
22-24 |
| Auxiliary rocket's characteristics |
|
|
| Velocity, m/s |
4500 |
4280 |
| 1st stage's characteristics |
|
|
| Lift off mass, kg |
47500 |
45950 |
| Empty mass, kg |
5500 |
7700 |
| 2nd stage's characteristics |
|
|
| Lift off mass (with the OS), kg |
15500 |
11970 |
| Empty mass, kg |
650 |
920 |
| OS's characteristics |
|
|
| Lift off mass, kg |
8800-10300 |
6800 |
| Empty mass, kg |
4190 |
4190 |
| Payload mass, kg |
500-2000 |
- |
| Ceiling, km |
130-150 |
130-150 |
