Which of these cannot be considered as design requirement of prop engine?(a) Range(b) Endurance(c) Take-off and landing(d) Turbine TemperatureI have been asked this question in an interview for job.This interesting question is from Conceptual Design Process in division Design Process Overview of Aircraft Design

Which of these cannot be considered as design requirement of prop engi

1.	Which of these cannot be considered as design requirement of prop engine?(a) Range(b) Endurance(c) Take-off and landing(d) Turbine TemperatureI have been asked this question in an interview for job.This interesting question is from Conceptual Design Process in division Design Process Overview of Aircraft Design
Answer» The correct choice is (d) Turbine Temperature For explanation I would say: A typical Prop ENGINE is reciprocating engine. Prop engine relies on the POWER produced through propeller. Range, take-off and landing, endurance etc. are affected by the power GENERATED by the Prop engine. If asked for Turbo-prop then, we can INCLUDE turbine as well.

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