Pull Up Maneuver Rate Calculator

The “Pull Up Maneuver Rate” typically refers to the rate at which an aircraft can ascend or climb during a pull-up maneuver. This rate is influenced by various factors, including the aircraft’s power, aerodynamic design, and the pilot’s input. A higher pull-up maneuver rate indicates a more rapid climb, and it is an important parameter for assessing the aircraft’s performance in dynamic maneuvers.

Where:

  • g is the gravity in m/s2.
  • n is the load factor.
  • v is the velocity in m/s.
  • ω is the Turn rate in rad/s.

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