Firework accommodating apparatus comprising a shaped body with an upwardly open recess and a first open bore at the bottom in the shaped body, which is situated centrally, wherein a second bore having a smaller diameter is preferably located next to the first bore, wherein in the first bore, preferably a continuous bore or hollow bore, preferably a rod, a so-called guide rod can be fastened and having at least two lateral cylindrical hollow bores in the shaped body or instead of the hollow bores, downwardly inclined wings.

A projectile having a fin deployment system disposed about its circumference. The fins are initially contained by a fin cover that is removed by aerodynamic force. The fins are then rotated around a rotational axis parallel to and offset from the central axial axis of the projectile body by the centrifugal forces created by the rotation of the projectile as the projectile passes through a barrel of a gun system or tube launcher. The fin deployment system can also have locking systems that lock the fins in the deployed position and prevent the fins from rotating back into the retracted position after deployment.

Firework accommodating apparatus comprising a shaped body with an upwardly open recess and a first open bore at the bottom in the shaped body, which is situated centrally, wherein a second bore having a smaller diameter is preferably located next to the first bore, wherein in the first bore, preferably a continuous bore or hollow bore, preferably a rod, a so-called guide rod can be fastened and having at least two lateral cylindrical hollow bores in the shaped body or instead of the hollow bores, downwardly inclined wings.

An aeromechanically stable sabot system that includes a center of gravity that is placed forward of an aerodynamic center of the aeromechanically stable sabot system when in steady-state flight. By placing the center of gravity forwards of the aerodynamic center, the sabot system exhibits positive longitudinal and directional stability. To illustrate, the sabot system and/or portions thereof will return to stable flight after being disturbed in pitch (vertically or about a transverse horizontal axis) or yaw (side to side or about a vertical axis) when traveling horizontally.

An aeromechanically stable sabot system that includes a center of gravity that is placed forward of an aerodynamic center of the aeromechanically stable sabot system when in steady-state flight. By placing the center of gravity forwards of the aerodynamic center, the sabot system exhibits positive longitudinal and directional stability. To illustrate, the sabot system and/or portions thereof will return to stable flight after being disturbed in pitch (vertically or about a transverse horizontal axis) or yaw (side to side or about a vertical axis) when traveling horizontally.