ReactionTurbines

Create new

Search in text fields: | Items per page

Name Family Aircraft Engine Manufacturer Aircraft Engine Type Comment Dry Weight Full Weight Diameter Length Height Width Control System List Price Program launch FETT First Flight Certification Production Start Production End Service End Number Built Fan Stages Fan Blades Fan Technology Geared Fan Gear Reduction Ratio Low-Pressure Compressor Stages Low-Pressure Compressor Technology Intermediary-Pressure Compressor Stages Intermediary-Pressure Compressor Technology High-Pressure Compressor Stages High-Pressure Compressor Technology Combustion Chamber High Pressure Compressor Stages High-Pressure Turbine Technology Intermediary-Pressure Turbine Stages Intermediary-Pressure Turbine Technology Low-Pressure Turbine Stages Low-Pressure Turbine Technology Afterburner Streams Bypass Ratio MaximumTakeoffThrust MaximumContinuousThrust MaximumClimbThrust MaximumCruiseThrust FlightIdleThrust ApproachIdleThrust GroundIdleThrust OEU30sec OEI2min OEI2min5 OEIContinuous OverallPressureRatio FanPressureRatio CompressorPressureRatio T3 T4 T9 BPMaxRotationSpeed IPMaxRotationSpeed HPMaxRotationSpeed MaxRotatingDiameter ThrustToWeight SpecificFuelConsumption Fuel TBO Modules HydrocarbonTakeOff HydrocarbonClimbOut HydrocarbotApproach HydrocarbonIdle HydrocarbonUnitaryAverage HydrocarbonUnitarySigma HydrocarbonUnitaryRange HydrocarbonUnitaryCharacteristic HydrocarbonUnitaryCharacteristictoRegulatory HydrocarbonLTO CarbonMonoxideTakeOff CarbonMonoxideClimbOut CarbonMonoxideApproach CarbonMonoxideIdle CarbonMonoxideUnitaryAverage CarbonMonoxideUnitarySD CarbonMonoxideUnitaryRange CarbonMonoxideUnitaryCharacteristic CarbonMonoxideUnitaryCharacteristictoRegulatory NOxTakeOff NOxClimbOut NOxApproach NOxIdle NOxUnitaryAverage NOxUnitarySD NOxUnitaryRange NOxUnitaryCharacteristic NOxUnitarytoStandard NOxUnitarytoCAEP2 NOxUnitarytoCAEP4 NOxUnitarytoCAEP6 NOxUnitarytoCAEP8 NOxLTO SmokeTakeOff SmokeClimbOut SmokeApproach SmokeIdle SmokeMax SmokeSigma SmokeRange SmokeCharacteristic SmokeCharacteristictoRegulatory FuelFlowTakeOff FuelFlowClimbout FuelFlowApproach FuelFlowIdle FuelLTO FuelVentingCompliant
AE3007A2 Rolls-Royce Turbofan No Type 3 (reduced emissions) No 2 4.79 42.23 20.20 0.00 0.00 0.00 1.71 3.45 5.32 27.12 146.00 0.71 0.74 4.08 73.29 89.96 76.24 18.61 15.99 7.90 4.39 43.03 49.88 62.04 77.55 81.66 83.78 90.80 1817.00 0.01 0.01 0.01 0.01 0.01 0.01 0.04 0.47 0.39 0.14 0.06 189.00 No
AE3007C2 Rolls-Royce Turbofan No Type 2 No 2 4.99 32.73 17.44 0.00 0.01 0.22 2.57 5.94 9.15 46.68 194.80 0.00 0.00 1.97 53.40 65.55 55.55 21.25 18.11 6.56 3.14 40.54 46.99 70.25 78.44 80.12 80.88 86.15 1326.30 0.01 0.01 0.01 0.01 0.01 0.01 0.04 0.33 0.27 0.10 0.05 147.00 Yes
PS-90A2 Aviadvigatel Turbofan No 93-03-800 No 2 4.32 156.95 31.23 0.11 0.14 0.21 2.88 5.23 0.00 4,98-5,55 6.80 34.70 820.00 0.44 0.65 1.91 30.76 0.00 28,46-31,84 35.10 29.70 32.70 25.52 9.31 4.30 50.34 0.00 46,70-53,60 55.40 54.50 68.10 80.70 91.70 105.40 7902.00 15.45 16.24 12.12 1.17 16.24 0.00 14,75-17,96 17.60 0.80 1.38 1.12 0.49 0.17 590.00 No
PW814GA Pratt & Whitney Canada Turbofan No TALON X No 2 5.66 68.63 33.87 0.00 0.00 0.02 0.05 0.10 0.07 0.0-0.2 0.10 0.50 6.00 0.00 0.00 1.76 23.10 1.53 20.8-24.7 24.70 20.90 23.26 17.94 11.46 6.25 46.10 1.19 45.0-49.5 48.40 44.90 56.20 61.70 66.20 73.50 3168.00 0.30 0.20 0.20 0.20 0.30 0.11 0.0-0.5 0.30 1.10 0.67 0.55 0.19 0.07 256.20 Yes
PW815GA Pratt & Whitney Canada Turbofan No TALON X No 2 5.60 71.22 35.00 0.00 0.00 0.02 0.05 0.10 0.07 0.0-0.2 0.10 0.51 7.00 0.00 0.00 1.50 21.90 1.38 19.9-23.3 23.40 19.80 24.88 18.89 11.47 6.41 48.10 1.11 47.0-51.7 50.50 45.91 57.39 63.05 67.88 75.37 3422.00 0.30 0.20 0.20 0.20 0.30 0.11 0.0-0.5 0.30 1.15 0.70 0.57 0.20 0.07 264.00 Yes
CFM56-7B24/2 CFM International Turbofan No No 2 5.20 107.65 25.95 0.05 0.07 6.01 6.55 14.66 13.4-15.9 17.10 87.20 1576.00 1.38 4.30 30.32 94.03 88.4-100.0 101.70 86.20 16.63 13.23 6.72 4.08 32.86 32.7-33.2 34.80 37.90 47.30 57.50 65.40 78.40 3534.00 0.70 0.70 0.70 0.70 0.65 0.2-1.5 0.70 3.10 1.09 0.90 0.31 0.11 410.00 No
CFM56-7B26/2 CFM International Turbofan No No 2 5.10 116.99 27.80 0.03 0.06 4.73 5.88 12.21 11.1-13.4 14.20 72.70 1425.00 0.77 2.51 26.07 81.39 77.1-85.9 88.00 74.60 19.20 14.77 7.26 4.27 36.24 36.0-36.8 38.40 40.20 50.20 60.50 68.70 81.70 4233.00 0.70 0.70 0.70 0.70 0.71 0.3-1.6 0.70 3.10 1.20 0.99 0.33 0.11 438.00 No
CFM56-7B22/2 CFM International Turbofan No No 2 5.30 100.97 24.61 0.06 0.10 6.06 7.26 16.31 14.6-18.2 19.00 97.10 1643.00 2.18 6.58 30.87 104.18 96.9-111.7 112.70 95.50 15.08 12.16 6.37 3.94 30.63 30.4-30.9 32.40 36.40 45.40 55.60 63.10 76.20 3091.00 0.70 0.70 0.70 0.70 0.69 0.1-1.8 0.80 3.20 1.01 0.84 0.30 0.11 389.00 No
AE3007A3 Rolls-Royce Turbofan No Type 1 No 2 4.72 33.00 17.20 0.23 0.27 0.69 4.71 10.93 14.22 72.60 361.00 0.83 1.03 4.22 59.41 67.69 57.40 18.52 15.79 6.83 3.38 39.87 43.84 58.90 73.70 75.30 76.10 81.10 1316.00 1.00 0.01 0.01 0.01 1.00 1.17 3.60 0.36 0.30 0.11 0.04 150.00 No
AE3007C Rolls-Royce Turbofan No No 2 5.30 28.60 16.20 0.29 0.33 0.83 5.84 13.46 17.50 89.30 387.00 0.97 1.19 4.50 68.00 77.50 65.70 16.92 14.56 6.63 3.24 34.73 38.20 52.80 66.00 66.40 66.60 70.40 991.00 1.00 0.00 0.00 0.00 1.00 1.20 3.60 0.28 0.23 0.09 0.04 125.00 No