Method for programming the shattering of projectiles and tube weapon with programming system
A method for programming the shattering of projectiles (G) and a weapon ( 12 ) with a programming system ( 14, 16, 18 ). The projectiles are intended to destroy a target (Z) at which they are fired along heavily curved trajectories and are detonated at shattering points near the target. The longitudinal distance (x Z ) of the target from the weapon is measured and the elevation (λ) is adjusted for which a known muzzle velocity (v 0 ( 0 )) and a longitudinal distance of the shattering point at a predetermined optimal height (y*) are taken into consideration. The actual muzzle velocity (v 0 (eff)) is determined and a calculation for the programming is carried out in which the actual muzzle velocity is taken into account and the optimal height of the shattering point is held constant. The corresponding programming is transmitted to the projectiles. The weapon has an associated programming system for correspondingly programming the projectiles. The programming system has v 0 -measuring means ( 14 ) for determining the actual muzzle velocity, and computer means ( 16 ) for calculating the programming of the projectiles, as well as transmitting means for transmitting the programming to the projectiles.
1. A method for programming the shattering of projectiles (G), which are intended for the destruction of a target (Z) and are to be shot from the tube ( 13 ) of a weapon ( 12 ) along a strongly curved trajectory (g, g*) to detonate at a shattering point (Q*) in the neighborhood of the target (Z), wherein
a distance measurement for determining the longitudinal distance (x Z ) of the target (Z) from the weapon ( 12 ) is carried out,
the tube ( 13 ) is adjusted to a suitable elevation (λ),
taking into consideration a predetermined muzzle velocity (v 0 ( 0 )) of the projectiles (G) and the longitudinal distance (x Z ) of the target (Z) from the weapon ( 12 ) as well as
maintaining an optimal height (y*) of the shattering point (Q*) above the target (Z)
an actual muzzle velocity (v 0 (eff)) of the projectiles (G) is determined,
a calculation for the programming is carried out
taking into consideration the actual muzzle velocity (v 0 (eff)) and
under the condition of maintaining the optimal height (y*) of the shattering point (Q*) above the target (Z), and
the programming is transmitted to the involved projectiles (G).
2. A method according to claim 1 , wherein for the calculation of the programming of the projectile (G) is carried out by
a preliminary calculation taking into consideration the predetermined muzzle velocity (v 0 ( 0 )) and
an ultimate calculation taking into account the actual muzzle velocity (v 0 (eff)).
3. A method according to claim 1 , wherein the projectiles (G) have a descent angle relative to the horizontal which exceeds the range of 5°.
4. A method according to claim 1 , wherein the flight paths (g, g*) of the projectiles (G) lie in the lower angle group.
5. A method according to claim 1 wherein the projectiles (G) are shot individually or in series.
6. A weapon ( 12 ) with a tube ( 13 ) for the shooting of projectiles (G) along heavily curved trajectories (g, g*) and with a programming system ( 14 , 16 , 18 ) for so programming the projectiles (G) that they detonate in flight at a shattering point (Q*) to destroy a target (Z) which is spaced from the weapon ( 12 ) by a longitudinal distance (x Z ), which programming system includes:
v 0 measuring means ( 14 ) for determining the actual muzzle velocity (v 0 (eff)) of the projectiles (G),
computer means ( 16 ) for calculating the programming of the projectiles (G)
taking into consideration a predetermined muzzle velocity (v 0 ( 0 )) of the projectiles (G) and the longitudinal distance (x Z ) of the target (Z) from the weapon ( 12 ), and
maintaining the optimal height (y*) of the shattering point (Q*) above the target (Z), and
taking into consideration the measured muzzle velocity (v 0 (eff)) of projectile (G), as well as
transmission means ( 18 ) for transmitting the programming to the projectiles (G).
7. A weapon ( 12 ) with a programming system ( 14 , 16 , 18 ) according to claim 6 , wherein the computer means ( 16 ) are constructed to,
carry out a precalculation taking into the account the predetermined muzzle velocity (v 0 ( 0 )),
carry out an ultimate calculation taking into account the actual muzzle velocity (v 0 (eff)), and wherein
the computer means ( 16 ) has associated storage means for storing the results of the precalculation up to the ultimate calculation.
8. A weapon ( 12 ) with a programming system ( 14 , 16 , 18 ) according to claim 6 wherein the projectiles (G) are so constructed and fireable that their descent angle relative to the horizontal exceeds the range of 5°.
9. A weapon ( 12 ) with a programming system ( 14 , 16 , 18 ) according to claim 6 wherein the projectiles (G) are fireable along trajectories (g, g*) which lie in the lower angle group.
10. A weapon ( 12 ) with a programming system ( 14 , 16 , 18 ) according to claim 6 wherein the weapon ( 12 ) is so constructed that the projectiles (G) are fireable individually or in series.