Missile having rotor ring

Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage

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Details

244 323, 102208, F42B 1002

Patent

active

049645935

ABSTRACT:
A missile having a rotor ring, which has at least one adjustable fin actuated by the relative rotation between the rotor ring and the missile. At least one motor is arranged between the rotor ring and the missile, and a control device is provided which allows the motor to work as a generator and performs the fin adjustment.

REFERENCES:
patent: 4076187 (1978-02-01), Metz
patent: 4426048 (1984-01-01), Mildren
patent: 4512537 (1985-04-01), Sebestyen et al.
patent: 4565340 (1986-01-01), Bains

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