Microturbo TRI 60

Turbojet · Microturbo
Reaction Turbines
Maximum Takeoff Thrust
5.7 kN
Diameter
343 mm
Length
841 mm
Dry Weight
61.2 kg
Thrust To Weight
9.53

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 annular
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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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
Aérospatiale C.22 Microturbo TRI 60 1 5.25 2.5

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN)
Garrett F109 Garrett 5.92 Compare
Heinkel HeS 8 Heinkel-Hirth 6 Compare
Power Jets WU Power Jets 6.18 Compare
All data (15 fields)
Name
Microturbo TRI 60
Aircraft Engine Manufacturer
Microturbo
Aircraft Engine Type
Turbojet
Dry Weight (kg)
61.2
Diameter (mm)
343
Length (mm)
841
Wikipedia Article (URL)
en.wikipedia.org/wiki/Microturbo_TRI_60
Geared Fan
No
Combustion Chamber
annular
Afterburner
No
Streams
1
Maximum Takeoff Thrust (kN)
5.7
Thrust To Weight
9.53
Compressor Description
4 stage axial
Turbine Description
single stage