![]() The first hotfire-tested BE-4, serial number 103, at the 34th Space Symposium in Colorado Springs in April 2018, showing the liquid methane inlet side of the engine | |
Country of origin | United States |
---|---|
First flight | January 8, 2024 |
Designer | Blue Origin |
Manufacturer | Blue Origin |
Associated LV | Vulcan Centaur New Glenn |
Predecessor | BE-3[1] |
Status | In production |
Liquid-fuel engine | |
Propellant | LOX / CH4 |
Cycle | Oxygen-rich staged combustion |
Performance | |
Thrust, sea-level | 2,400 kN (550,000 lbf) |
Throttle range | 40–100% |
Chamber pressure | 140 bar (14,000 kPa) |
Specific impulse | 340 s (3.3 km/s)[2] |
Burn time | 299 seconds (Vulcan)[3][4] |
Gimbal range | ±5° |
The BE-4 (Blue Engine 4)[5] is an oxygen-rich,[6] liquefied-methane-fueled, staged-combustion, rocket engine. It is produced by Blue Origin. BE-4 was developed with private and public funding.[7] The engine produces 2,400 kilonewtons (550,000 lbf) of thrust at sea level.[8]
The engine was initially planned to be used exclusively on Blue Origin's proprietary New Glenn launch vehicle. However, in 2014 United Launch Alliance (ULA) selected the engine for the Vulcan Centaur launch vehicle, the successor to the Atlas V launch vehicle.[9] ULA's final engine selection happened in September 2018.[10]
BE-4's first flight test of the new engine launched on 8 January 2024 on the Vulcan Centaur rocket.
wp201409
was invoked but never defined (see the help page).ars20160309
was invoked but never defined (see the help page).