| Characteristic |
Value |
|
Winged version |
Lifting body version |
Hybrid version |
| Mass |
|
| Capsule, t |
16 |
17 |
15 |
| Recovery system, t |
5.5 |
5.7 |
5.4 |
| Orbit |
|
| Initial orbit, km |
130 x 170 |
| Working orbit, km |
440 x 440 |
| Free volume per people, m³ |
2.2 |
2 |
2 |
| Accelerations |
|
| Nominal, g |
2.5 |
| During descent, g |
5 |
1-2 |
1-2 |
| After a failure of the launcher, g |
up to 8.5 |
up to 6.5 |
up to 8.5 |
| Lateral cross range, km |
500 |
1 200 |
500 |
| Cross range in the orbit, km |
6 000 |
13 000 |
6 000 |
| Landing precision, km |
inferior to 11 |
0 |
0 |
| Reusability coefficient |
~0.8 |
up to 1 |
up to 1 |
| Number of orbits per day which allow to land in Russia |
3-4 |
9 |
7 |
| Payload's mass, kg |
|
| With a crew of 6 |
500 |
| With a crew of 2 |
1000 |
| Crew |
6 |
