Saboted projectile

Ammunition and explosives – Projectiles – Composite

Patent

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Details

F42B 1406

Patent

active

051824191

ABSTRACT:
A saboted projectile comprises a sub-caliber, spin-stabilized warhead (usually an armor-piercing penetrator) and a full caliber spin-stabilized non-disintegrating sabot capable of being fired by airplanes. The sabot releasably receives the armor-piercing penetrator and is adapted to be mounted on a conventional ammunition cartridge. The sabot includes a novel method of holding the penetrator until firing, tightening a reverse threaded end cap against the aft end of the penetrator during firing and utilizing interior end cap geometry to utilize firing gas pressure to accelerate the penetrator forward in relation to the sabot after leaving the gun barrel. Accuracy is increased by maintaining axial symmetry and releasing the penetrator in substantially the same way each time. There are other novel features.

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Engineering Design Handbook, Design for Control of Projectile Flight Characteristics Sep. 1966.
Ordinance Engineering Design Handbook, Artillery Ammunitions Series, Section 3, May 1977, Design for Control of Flight Characteristics.
Exterior Ballistics, Shane, Kelly and Reno 1953, Chapter 11.

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