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For estimated value of the thrust loading, we got three different values of wing loading. As a designer typically which wing loading should be considered?

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For estimated value of the thrust loading, we got three different values of wing loading. As a designer typically which wing loading should be considered?

(a) Lowest among all three

(b) Highest among all three

(c) Any value

(d) Always take average

The question was posed to me in an online quiz.

Enquiry is from Selection of Thrust-Weight and Wing Loading in portion Thrust-Weight Ratio and Wing Loading of Aircraft Design

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Correct answer is (a) Lowest among all three

The best I can explain: In general, we chose the lowest among all the values. This is done if and only if the lowest value can satisfy almost every mission phase requirement; from take-off to land. If it does not satisfy then, we should estimate another value.

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