Turbomeca Gabizo

 The Turbomeca Gabizo was a small turbojet engine produced by Turbomeca and first run in 1954. The components were designed to take the stresses of high-speed fighter aircraft with some variants featuring afterburner.

Applications:
Fouga CM.171 Makalu
Dassault Étendard II
SNCASO Trident

Specifications:
Gabizo
Type: Turbojet
Length: 86 in (218.4 cm)
Diameter: 26.5 in (67.3 cm)
Dry weight: 560 lb (254.0 kg)
Compressor: Single stage axial plus single-stage centrifugal
Combustors: Single annular combustion chamber
Turbine: Single-stage
Maximum thrust: 2,426 lbf (10.78 kN)(maximum thrust) 1,940 lbf (8.62 kN)(maximum continuous thrust)
Overall pressure ratio: 5.1:1
Specific fuel consumption: 1.04
Thrust-to-weight ratio: 4.332 lbf/lb (0.042 kN/kg)