West Engineering XJ38

Dry Weight
81.6466 kg
Thrust To Weight
1.31

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 Single reverse flow
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 No

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All data (12 fields)
Name
West Engineering XJ38
Aircraft Engine Manufacturer
West Engineering
Aircraft Engine Type
Turbojet
Dry Weight (kg)
81.6466
Wikipedia Article (URL)
en.wikipedia.org/wiki/West_Engineering_XJ38
Geared Fan
No
Combustion Chamber
Single reverse flow
Afterburner
No
Streams
1
Thrust To Weight
1.31
Compressor Description
Centrifugal
Turbine Description
Single stage