The two main sources of information used to calculate turbojet thrust are the:

Question

Question ATPL - Airline Transport Pilot license - Aircraft General Knowledge - Instrumentation

QuizVDS · Accepted Answer

Fan rotation speed (or N1) or the EPR (Engine Pressure Ratio).

QuizVDS · Answer

Fan rotation speed (or N1) or the total pressure at the low pressure turbine outlet.

QuizVDS · Answer

Fan rotation speed (or N1) or the total pressure at the high pressure compressor outlet.

QuizVDS · Answer

High pressure turbine rotation speed or the EPR (Engine Pressure Ratio).

Id 199 - ATPL - The two main sources of information used to calculate turbojet thrust are the: