Brandner E-300

Turbojet · Brandner
Reaction Turbines
Maximum Takeoff Thrust
32.4 kN
Diameter
840 mm
Length
4300 mm
Dry Weight
860 kg
Thrust To Weight
3.31

Architecture

Fan Fan Stages — Fan Blades — Fan Technology — Fan Pressure Ratio —
Gearbox Geared Fan No Gear — Reduction Ratio —
LP compressor Low-Pressure Compressor Stages — Low-Pressure Compressor Technology — BP Compressor Pressure Ratio —
IP compressor Intermediary-Pressure Compressor Stages — Intermediary-Pressure Compressor Technology — IP Compressor Pressure Ratio —
HP compressor High-Pressure Compressor Stages — High-Pressure Compressor Technology — HP Compressor Pressure Ratio —
Combustor Combustion Chamber can-annular combustion chamber
HP turbine High Pressure Compressor Stages — High-Pressure Turbine Technology —
IP turbine Intermediary-Pressure Turbine Stages — Intermediary-Pressure Turbine Technology —
LP turbine Low-Pressure Turbine Stages — Low-Pressure Turbine Technology —
Whole engine Streams 1 Bypass Ratio — Overall Pressure Ratio — Afterburner Yes

Pictures

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All data (15 fields)
Name
Brandner E-300
Aircraft Engine Manufacturer
Brandner
Aircraft Engine Type
Turbojet
Dry Weight (kg)
860
Diameter (mm)
840
Length (mm)
4300
Wikipedia Article (URL)
en.wikipedia.org/wiki/Brandner_E-300
Geared Fan
No
Combustion Chamber
can-annular combustion chamber
Afterburner
Yes
Streams
1
Maximum Takeoff Thrust (kN)
32.4
Thrust To Weight
3.31
Compressor Description
nine-stage axial compressor
Turbine Description
two-stage axial turbine