SpaceX Mars Rocket Engine Simulation
Raptor Engine Specifications
Thrust (sea level):
2,200 kN (500,000 lbf)
Thrust (vacuum):
2,600 kN (580,000 lbf)
Specific impulse (sea level):
330 s
Specific impulse (vacuum):
380 s
Chamber pressure:
300 bar (4,350 psi)
Simulation Features
Real-time combustion dynamics
Propellant flow visualization
Thermal analysis of engine components
Nozzle expansion ratio optimization
Turbopump performance metrics
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