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Which of the following best explains why a rocket nozzle is designed for a particular altitude?

  • A.The specific heat ratio varies with altitude
  • B.The throat area must change with altitude
  • C.Ambient pressure varies with altitude
  • D.The stagnation temperature varies with altitude

Answer: C

The area ratio fixes the exit pressure, but the ambient pressure falls steadily as the vehicle climbs, so the two can match at only one altitude. A first stage is therefore overexpanded at sea level and underexpanded high up, and the design altitude is chosen to minimise the total loss over the trajectory.

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