Projectile having circumferential members for varying a base...

Ammunition and explosives – With extendable arms

Reexamination Certificate

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Details

C102S490000, C102S501000, C244S003240, C244S003260, C244S003270

Reexamination Certificate

active

11178750

ABSTRACT:
A method for enhancing an aerodynamic performance of an unmanned projectile. The method including at least one of the following: (a) morphing a cross-sectional shape of the projectile after launch thereof; (b) morphing a longitudinal shape of the projectile after launch thereof; (c) bleeding a fluid at a base of the projectile during flight thereof: (d) varying a base cone angle of the projectile as a function of speed thereof; (e) deploying at least one wing from a body of the projectile after launch thereof; and (f) deploying a fin from the body of the projectile after launch thereof.

REFERENCES:
patent: 3412962 (1968-11-01), Killian
patent: 3492911 (1970-02-01), Adams
patent: 3572250 (1971-03-01), Kriesel et al.
patent: 4215836 (1980-08-01), Zacharin
patent: 4674706 (1987-06-01), Hall
patent: 6297486 (2001-10-01), Rom et al.
patent: 6783095 (2004-08-01), King et al.
patent: 6923123 (2005-08-01), Rastegar et al.

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