SpaceX Investor Event Presentation Deck

Cycle Oxidizer Fuel Chamber Pressure Throttle Capability Sea-Level Nozzle Full-flow staged combustion Subcooled liquid oxygen Subcooled liquid methane 300 bar 20% to 100% thrust Expansion Ratio: 40 Thrust (SL): 3,050 kN Isp (SL): 334 s Vacuum Nozzle Expansion Ratio: 200 Thrust: 3,500 kN Isp: 382 s

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