SRM
|
Z9A SRM |
Z23 SRM |
P80 SRM |
Note |
| Thrust [kN] |
297,205 |
1122,505 |
3015,0108 |
[5] |
| Burning time [s] |
118,5 |
77,7 |
109,8 |
[3] |
| Mass [kg] |
11485,4 |
25756 |
95020,9 |
[2] |
| Propellant Mass [kg] |
10570,3 |
23823,4 |
87733 |
[1] |
| Total Impulse [kN s] |
30672 |
67126 |
240470 |
[4] |
| MR |
0,92 |
0,925 |
0,923 |
[2] |
[1] Including igniter propellant mass
[2] For P80 SRM total mass includes TVC subsystems
[3] Burning time (action time T38, 1.5 BAR)
[4] Action time vacuum total impulse (up to T38)
[5] Maximun vacuum thrust
|
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