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Which of these cannot be considered as design requirement of prop engine?

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Which of these cannot be considered as design requirement of prop engine?

(a) Range

(b) Endurance

(c) Take-off and landing

(d) Turbine Temperature

I 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

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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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