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| Raptor-2 rocket engine |
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Engines |
Nozzle area |
Chamber | Propellant |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Flow rate |
| ratio (AR) | pressure | mix | kN | N*s/kg | kN | N*s/kg | t/s | |
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Raptor-2 |
1:24 | 32.1 MPa | 2.60 | ~2,400 |
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Raptor-2 is intended to replace the problematic Raptor engines. Raptor-2 is an upgraded Raptor engine. Combustion chamber (including throat) conforms to the Raptor-vac engine (RVAC). |
