Projectile

Details Projectile Projectile

1975-01-02

1976-12-07

Pendegrass, Verlin R.

Ammunition and explosives

Igniting devices and systems

244 31, F42B 1300

Patent

active

039955583

ABSTRACT:
A projectile having mainstream air flow directed to its surface region of rmal air non-attachment during operational flight and in which drag frictional forces in the laminar flow boundary layer region are minimized to produce maximum range. The projectile conical nose has a forward air intake nozzle in fluid communication with a plurality of internal passageways that terminate in outlet ports circumferentially spaced along the rearmost edge of the nose member adjacent the forwardmost external or lateral surface of the projectile main body portion.

REFERENCES:
patent: 2941469 (1960-06-01), Barnhart
patent: 3129667 (1964-04-01), Wen
patent: 3485460 (1969-12-01), Mertens

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