Ammunition and explosives – Projectiles – Composite
Patent
1986-09-16
1988-07-05
Tudor, Harold
Ammunition and explosives
Projectiles
Composite
102524, F42B 3100
Patent
active
047547073
ABSTRACT:
A projectile which is fireable in a spin-stabilized manner from a weapon barrel or launch tube through the action of the gas pressure generated by a propellant charge, and which projectile is guidable during flight. The projectile is equipped in the rearward region of its tail-end structure, and preferably behind the control surfaces, with a type of propulsion cage so as to, through the intermediary of the gas pressure generated by the propellant charge, faciliate a ballistic firing of the projectile from a weapon barrel or launch tube. The projectile is equipped with a sealing ring, which with a gliding frictional contact, coaxially encompasses an axially-limited region of the tail-end structure of the projectile.
REFERENCES:
patent: 2809587 (1957-10-01), Musser
patent: 2928348 (1960-03-01), Zisman et al.
patent: 3738279 (1973-06-01), Eyre et al.
patent: 3834314 (1974-09-01), Young
patent: 4109582 (1978-08-01), Halp et al.
patent: 4242961 (1981-01-01), Moredock et al.
patent: 4366015 (1982-12-01), Murray
patent: 4520731 (1985-06-01), Gotz et al.
patent: 4552071 (1985-11-01), Horais
Diehl GmbH & Company
Tudor Harold
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