Turbomeca Gabizo

Turbojet · Turbomeca
Reaction Turbines
Diameter
670 mm
Length
2083 mm
Dry Weight
265 kg
Thrust To Weight
4.15
Specific Fuel Consumption
28.325 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 Single 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 No

Pictures

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
Bréguet 1100 Turbomeca Gabizo 2 12.52 7.83
Dassault Étendard II Turbomeca Gabizo 2 12.89 8.74
SNCASO SO.9000 Trident Turbomeca Gabizo 2 12.7 6.98
All data (16 fields)
Name
Turbomeca Gabizo
Aircraft Engine Manufacturer
Turbomeca
Aircraft Engine Type
Turbojet
Dry Weight (kg)
265
Diameter (mm)
670
Length (mm)
2083
Wikipedia Article (URL)
en.wikipedia.org/wiki/Turbomeca_Gabizo
Fuel
Aviation kerosene / JP-1
Geared Fan
No
Combustion Chamber
Single annular combustion chamber
Afterburner
No
Streams
1
Thrust To Weight
4.15
Specific Fuel Consumption (g/(kN·s))
28.325
Compressor Description
Single stage axial plus single-stage centrifugal
Turbine Description
Single-stage axial