To provide a treatment method for a propellant and projectile which is capable of safely executing a large amt. of the propellant and projectile to a combustion treatment in a short period of time in an opened environment and is extremely high in workability and treatment efficiency.
The propellant or projectile is formed by adhering, absorbing or dissolving additives for incineration having a viscosity of 0.5 to 400cPs, more preferably 0.5 to 200cPs to the solid propellant and projectile in the form of a single holed pipe, perforated pipe or bar by spraying, dipping, etc., and treating such propellant and projectile by burning. As a result, the overall combustion of the propellant and projectile is derived from the start of combustion. In addition, the lowering of the combustion temp. or combustion speed of the propellant and projectile is made possible. Then, the flying of the propellant and projectile and the generation of explosive sounds and splashes at the time of the burning treatment of the propellant and projectile are sufficiently prevented and the combustion treatment of a large amt. of the propellant and projectile is safely executed in the short period of time in the opened environment.
UYAMA MASAHIRO
KOBAYASHI GORO
