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Typically, designer designs thrust loading based on ________

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Typically, designer designs thrust loading based on ________

(a) static sea-level conditions, take-off requirement etc

(b) only Lift

(c) only static sea-level conditions

(d) only landing conditions

The question was asked during an internship interview.

This intriguing question originated from Thrust Weight Ratio-1 in division Thrust-Weight Ratio and Wing Loading of Aircraft Design

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The correct option is (a) static sea-level conditions, take-off requirement etc

The explanation: When designer speaks for a thrust loading it generally refers to the value which has been calculated for standard day conditions, static sea-level conditions, take-off performance etc. Different phases incorporate different values of thrust loading. Hence, a designer typically converts them to take-off conditions.

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