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An engine burns \( 0.9 \ \mathrm{kg/s} \) of fuel producing \( 50 \ \mathrm{kN} \) of thrust. Its thrust specific fuel consumption is

  • A.\( 45 \ \mathrm{g/(kN\,s)} \)
  • B.\( 1.8 \ \mathrm{g/(kN\,s)} \)
  • C.\( 18 \ \mathrm{g/(kN\,s)} \)
  • D.\( 55.6 \ \mathrm{g/(kN\,s)} \)

Answer: C

Dividing gives \( 0.9/50 = 0.018 \) kilograms per kilonewton second. This is the figure that dominates a transport aircraft's operating cost, which is why decades of development went into reducing it through higher bypass ratios and pressure ratios.

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