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Three of the following are typical of a fighter rather than a transport. Which is not?

A thrust-to-weight ratio near 0.28

A sustained turn constraint

A thrust-to-weight ratio near unity

A design point set by manoeuvre rather than field length

  • A.A thrust-to-weight ratio near 0.28
  • B.A sustained turn constraint
  • C.A thrust-to-weight ratio near unity
  • D.A design point set by manoeuvre rather than field length

Answer: A

Correct answer: A thrust-to-weight ratio near 0.28

A thrust-to-weight ratio near \( 0.28 \) is typical of a transport, not a fighter. Transports cruise efficiently at high lift-to-drag ratios and need thrust chiefly for takeoff and engine-out climb, so values around \( 0.25 \) to \( 0.35 \) are usual.

The other three are characteristic of fighters. A sustained turn constraint appears only where hard manoeuvring is required; a thrust-to-weight near unity follows from it, since \( T/W \approx n/(L/D) \) gives large values at high load factor; and a design point set by manoeuvre rather than field length is the natural consequence.

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