Ho-301 cannon

The caseless design revolved around a specially designed projectile, that was in effect a small rocket. 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 base plate of the round are twelve 3.8 millimeter 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. 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. The modern Russian VOG grenades fired by the GP-25 grenade-launcher use a similar principle.

• Name — Ho-301 40 mm cannon • Origin — Japan • Type — Aircraft autocannon • Is Ranged — yes • Used By — Japan • Wars — Second World War • Weight — 49 kg (108 lb) • Length — 1486 mm • Part Length — 780 mm • Cartridge — 40 mm caseless (590g) • Caliber — 40 mm (1.57 in) • Action — API blowback • Rate — 475 rounds/min • Velocity — 245 m/s (805 ft/s) • Range — 150 meters (490 ft) • Feed — 10 round box

• Length of projectile (fuzed): 129 mm • Diameter of rotating band: 41 mm • Diameter of body: 39 mm • Wall thickness: 4 mm - 5 mm • Weight: 0.590 kg • Explosive content: 0.065 kg approx • Fuze: Direct acting impact fuze