The invention is useful for igniting a propellant charge of ammunitions.

The invention concerns an igniter tube (1), in particular for propellant charge (4) of an artillery ammunition (2), consisting of a tubular body (8) for receiving an igniting composition (14).

The ammunition according to the invention comprises a case consisting of a cylindrical envelope (2) carrying at each end a cap (3a, 3b), and within which are disposed a projectile (8) and a propellant charge.

The tubular body (8) comprises at least a receiving surface (25) oriented so as to receive the propellants generated when the propellant charge (4) is ignited, the propellants thereby driving the igniter tube (1).

The invention is useful for igniting a propellant charge of ammunitions.

The powertrain is intelligently packaged in such a way that its installation has no impact on the H350’s load area.

The invention concerns an igniter tube (1), in particular for propellant charge (4) of an artillery ammunition (2), consisting of a tubular body (8) for receiving an igniting composition (14).

The bore is filled above the primer charge with a propellant and above the propellant with a payload.

Meanwhile the propellant structure comprises an oxidizer rich layer (220b) which also contains fuel and a layer (220a).

propulsion machinery order

In this manner, the propellant is caused to burn in controlled, uniform manner.

The propellant layer (220a) consists of fibrous nitrocellulose.

The lubricant is incorporated in the propellent of the turbomachine.

The ammunition according to the invention comprises a case consisting of a cylindrical envelope (2) carrying at each end a cap (3a, 3b), and within which are disposed a projectile (8) and a propellant charge.

Consolidated propellant charge base thereon.