| Rocket total mass |
155000 |
kg |
|
155000 |
kg |
|
|
| Payload mass |
1200 |
kg |
|
503.29 |
kg |
|
2.384311 |
| Achieved
velocity |
11.2 |
km/s |
|
13.202 |
km/s |
|
|
| Propellant
mass |
153800 |
kg |
|
154496.7 |
kg |
|
|
4.861104 |
|
5.730014 |
|
| Average
propellant speed |
2.304004 |
km/s |
|
2.304008 |
km/s |
|
|
| Soyuz start
mass |
313 |
tonnes |
|
| Soyuz dry
weight |
26.5 |
tonnes |
|
|
| Falcon V
start mass |
155000 |
kg |
|
| out of which |
141877 |
kg is fuel |
|
| out of which |
39853.09 |
kg is kerosine |
|
|
1713683 |
MDj |
|
|
1.71E+12 |
Dj |
|
|
| Payload mass |
1200 |
kg at 200 km orbit |
|
| impulse |
11200 |
m/s |
|
| or |
7.53E+10 |
Dj |
|
|
| Efficiency |
4.3919% |
|
|
| Impulse |
11200 |
13202 |
1400.714 |
|
| Propellant speed |
2304.008 |
2304.008 |
2304.008 |
|
|
4.861093 |
5.730014 |
0.607947 |
|
| e = |
2.718282 |
2.718282 |
2.718282 |
|
|
129.1654 |
307.9735 |
1.836656 |
|
| Efficiency |
0.774% |
0.325% |
54.447% |
|
|
|
|
|
|
|
|
|