Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1981-10-09
1983-06-07
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
102501, F42B 1300
Patent
active
043867472
ABSTRACT:
A projectile for use with a smooth bore barrel is disclosed wherein longitudinal stability is provided by an oscillating mass within the projectile. A mass is disposed inside the projectile and attached and secured to the projectile by means of a bi-convex spring or equivalent flexible structure so that the mass is set off in oscillation upon the sudden acceleration due to the firing of the projectile. The inertial forces developed by the oscillating mass provide stability throughout the projectile's trajectory.
REFERENCES:
patent: 18568 (1857-11-01), Bates
patent: 1316363 (1919-09-01), Hayden
patent: 3853062 (1974-12-01), Cole
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