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 conditionsThe 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

Typically, designer designs thrust loading based on ________(a) static

1.	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 conditionsThe 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
Answer» 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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