Ammunition and explosives – Igniting devices and systems
Patent
1973-12-06
1976-04-20
Jordan, Charles T.
Ammunition and explosives
Igniting devices and systems
102 921, 102 927, F42B 1346, F42B 1132
Patent
active
039510700
ABSTRACT:
A rotatable airfoil projectile comprising a hollow closed circular ring wing surrounding a central open area with a non-lethal riot control agent positioned within the hollow ring. The projectile consists of an aerodynamic lifting body of a thick ring wing geometry which uses spin imparted to it from a launching means for its gyroscopic stability. The combination of aerodynamic stability characteristics and high spin rate (i.e. above 2,000 rmp) results in a flat trajectory and extended range capability.
The projectile ruptures on impact due to centrifugal and impact forces to distribute the non-lethal riot control payload about the target area. The sub-sonic launch velocity avoids bodily harm due to impact with a person even at point-blank range.
REFERENCES:
patent: 3074344 (1963-01-01), Devaux
patent: 3170405 (1965-02-01), Jungermann et al.
patent: 3311061 (1967-03-01), Roehrdanz
patent: 3318033 (1967-05-01), Barr
patent: 3738271 (1973-06-01), La Costa
Flatau Abraham
Miller Miles C.
Olson Donald N.
Church Robert W.
Edelberg Nathan
Gibson Robert P.
Jordan Charles T.
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