Spin-stabilized training missile

Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control

Patent

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Details

244 324, 102529, F42B 1320

Patent

active

045209723

ABSTRACT:
A spin-stabilized training missile is equipped with a stabilizer device for reducing spinning in order to decrease the flight range. The training missile is designed so that its stabilization attainable solely by the spin upon firing is not sufficient for a stable flight in the practice range. The required additional stabilizing in the practice range is obtained by a stabilizer device or control airfoil effecting simultaneously, after leaving the practice range, such a spin reduction that the training missile becomes unstable and the range of flight is controlled.

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