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.