Projectile with correctable trajectory

Details Projectile with correctable trajectory Projectile with correctable trajectory

1990-09-10

1991-10-08

Hellner, Mark

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

102202, 102381, F42B 1518

Patent

active

050547127

ABSTRACT:
A spin-stabilized projectile with a correctable trajectory, wherein the projectile possesses lateral or transverse thrust-propulsion devices which are distributed about the circumference thereof, each incorporating an impulse-generating charge inclusive an electrically-activatable detonator arranged beneath a cover which is radially ejectable relative to the longitudinal axis of the projectile. The detonator, with the presence of a connecting cable which initially extends coaxially with the cover and then thereafter extends at an angle relative thereto, is arranged in the transitional region intermediate the impulse-generating charge and the cover, whereby the cover, with conformance of its external contour to the contour of the encompassing casing surface of the projectile, is fixed to the structure of the projectile across a rupture location, which is hermetically sealed radially inwardly of the impulse-generating charge with respect to the center of the projectile.

REFERENCES:
patent: 3034434 (1962-05-01), Swaim et al.
patent: 4211378 (1980-07-01), Crepin
patent: 4503773 (1985-03-01), Bolieau
patent: 4982913 (1991-01-01), Miller

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