Скачать или смотреть Evaluation of Aircraft Weapons Deployment

This Wind Tunnel test technique is used to define the flight characteristics and resulting trajectory of a weapon when it is released from the parent air vehicle into the surrounding flow field. Using Calspan’s 6-degree of freedom remote positioning system and on-line integration of equations-of-motion, aerodynamic measurements can be acquired from the test article(s) and incorporated with other physical forces (e.g., gravity, ejectors force, restraints, inertial properties, etc.) to map out the trajectory over time. Whether it is for internal or external carriage, specific release parameters for that weapon can be scrutinized for safety of release (i.e., clearance) and stability of flight.

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