Statement No.15
Once the Gross Thrust force has been delivered to the Aircraft/engine's mounting bolts which it is at all in flight demand conditions its job, purely as a physical engine is done.
At this point, the thrust demanded and it's capacity, s.f.c per unit of thrust, per pound of fuel per hour and, the efficiency or inefficiency all of it's engine's physical systems are accounted and paid for and, the potential speed, payload and Aircraft range determined limited only by the Aircraft's fuel capacity.
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