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BLUE ORIGIN

BE-4

ACTIVE
2,647 kN (595,000 lbf)THRUST VAC (kN)
330 sISP VAC (s)
Oxygen-Rich Staged CombustionCYCLE
Liquid Methane (CH₄)/LOXPROPELLANT
Apr 2026FIRST FLIGHT
ABOUT BE-4

The BE-4 is an oxygen-rich staged combustion cycle engine developed by Blue Origin, burning liquid methane and liquid oxygen. It powers the first stage of ULA’s Vulcan Centaur and Blue Origin’s own New Glenn rocket. The BE-4 represents a new generation of American-made engines designed to replace the Russian RD-180.

Image: Blue Origin
PERFORMANCE
Thrust (Sea Level)2,400 kN (540,000 lbf) kN
Thrust (Vacuum)2,647 kN (595,000 lbf) kN
ISP (Sea Level)300 s s
ISP (Vacuum)330 s s
Chamber Pressure13.4 MPa (1,943 psi) bar
Mass2 kg
Thrust-to-Weight122
Throttle Range40–100%
Restart CapableYes
THRUST CONVERSIONS (VACUUM)
Kilonewtons2.0 kN
Pounds-force450 lbf
ENGINE CYCLE
Oxygen-Rich Staged Combustion
PROPULSION
PropellantLiquid Methane (CH₄)
OxidizerLOX
Engine CycleOxygen-Rich Staged Combustion
Mixture Ratio3.6:1
Flow Rate~800 kg/s kg/s
PHYSICAL
Dimensions2.0 m diameter × 3.4 m length
Combustion Chambers1
Nozzle Expansion Ratio35:1:1
GENERAL
ManufacturerBlue Origin
CountryUnited States
StatusActive
First FlightApril 17, 2026
VARIANTS (1)
  • BE-4
VEHICLES USING BE-4 (2)
ENGINE LINEAGE
BE-3BE-4

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