Diameter
400.05 mm
Length
2639.06 mm
Specific Fuel Consumption
70.812 g/(kN·s)

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 —
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

Pictures

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All data (10 fields)
Name
Bristol Thor
Aircraft Engine Manufacturer
Bristol Engine Company (Bristol)
Aircraft Engine Type
Ramjet
Diameter (mm)
400.05
Length (mm)
2639.06
Wikipedia Article (URL)
en.wikipedia.org/wiki/Bristol_Thor
Geared Fan
No
Afterburner
No
Streams
1
Specific Fuel Consumption (g/(kN·s))
70.812