NAVWEPS 0040T-80 
AIRPLANE PERFORMANCE 
AFTERBURNER COMPONENTS 
AFTt$lRNRNER 
HOLDERS 
PRE -COMPRESSOR 
WATER INJECTION 
WATER INJECTION 
NOZZLES 
CHAMBER NOZZLE 
INJECTION 
TURBINE-PROPELLER COMBINATION 
REDUCTION 
TURBINES 
CHAMBER NOZZLE 
Figure 2.14. Thrust Augmentation and the Gas Turbine-Propeller Combination 
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