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| Propulsion Athena-III |
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Stage |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
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| kN | N*s/kg | kN | N*s/kg | tons | s | t/s | MN*s | |||||
| 1 | SRBM-2.5 | max | 9,274.0 | 2452 | max | 10,231.0 | 2705 | 344.278 | 113.2 | max | 3.7827 | 931.04 |
| ave | 7,459.1 | ave | 8,228.9 | ave | 3.0425 | |||||||
| 2 | Castor-120 | max | max | 1,868.5 | 2736 | 49.006 | 79.5 | max | 0.6828 | 134.07 | ||
| ave | ave | 1.685.9 | ave | 0.6162 | ||||||||
| 3 | Castor 30 | max | max | 348.5 | 2890 | 12.837 | 143 | max | 0.1207 | 37.10 | ||
| ave | ave | 258.9 | ave | 0.0896 | ||||||||
| O.A.M. | MR-107 (4) | 0.89 | 2206 | 0.354 | 890 | 0.0004 | 0.78 | |||||
