Prime power source and control for a guided projectile

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

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Details

F42B 1502

Patent

active

044388934

ABSTRACT:
In a projectile including a spinning main housing and a despun canard frame having deflectable canards thereon, a pair of stator windings are disposed within the main housing and a cooperating pair of rotors are arranged within the canard frame. The first stator windings and corresponding rotor generate prime power and permit control of the rotational position of the canard frame while the second stator windings and associated rotor allow control of the deflectable canards.

REFERENCES:
patent: 2920568 (1960-01-01), Rabinow
patent: 2990776 (1961-07-01), Clarke
patent: 3067681 (1962-12-01), Beman
patent: 3111088 (1963-11-01), Fisk
patent: 3125027 (1964-03-01), Stoller

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