Gun Wiki

M.O.S. Please read and keep the Manual of Style in mind while editing.

Also, remember that there is to be no copying and pasting from other sources, at any time - your edits must be in your OWN words!

READ MORE

Gun Wiki
Question book-new.svg
This article needs more links to other articles to help integrate it into the encyclopedia. Please help improve this article by adding links that are relevant to the context within the existing text. (September 2018)

The Ho-301 was a Japanese 40mm calibre autocannon that saw limited use during World War II, on the IJA's Nakajima Ki-44 and Kawasaki Ki-45 KAI aircraft. It was unusual in using a type of pseudo-caseless ammunition. Although the effective range of the cannon was only 150 meters (490 ft), the Ho-301 was light and rapid firing for its caliber.

Because of the low muzzle velocity (245 meters/second or about 804 ft/sec - equivalent to a moderately powerful air rifle) the weapon was only suited to attacking bombers; even here the extremely low muzzle velocity made it difficult to achieve hits from any position besides directly astern the target aircraft and well within the range of defensive counterfire.

Ammunition[]

The design revolved around a specially designed projectile which made use of the high/low principle of recoil mitigation. The round used an internal propellant chamber at the rear of the projectile containing a ten gram silk bag filled with smokeless powder. Drilled into the baseplate of the round are twelve 3.8mm diameter exhaust holes. The propellant chamber is sealed by a thin aluminum sealing cup, which covers the exhaust holes. When the primer is struck, the bag of propellant ignites, and the pressure rises until the aluminum cup bursts, allowing the exhaust gas to rush through the exhaust holes pushing the projectile forward. The propellant was exhausted before the projectile left the barrel.

References[]