The invention concerns a projectile, especially a training projectile, that can be fired from a weapon system with a fire control computer.
Training ammunition of this type is disclosed, for example, by DE 100 14 513 A1. Training ammunition with a flared tail piece with slots is described, for example, in U.S. Pat. No. 5,498,160. DE 90 12 031 U1 describes a flared tail piece with holes.
As is well known, modern weapon systems have a fire control computer, which is adapted to each type of weapon and ammunition. Therefore, when new varieties and types of ammunition are introduced, the fire control computer requires complicated adaptation. In addition, one of the main considerations for training ammunition is economy. The adaptation is usually carried out in a permanent location, so that the fire control computers, including vehicles or the like, must be brought to a predetermined site and thus also become unavailable for practice purposes.
The object of the present invention is to provide the possibility of adapting existing training ammunition with a flared tail piece and a fire control computer that is already present but not yet adapted to this training ammunition, and to allow this adaptation to be made in a way that takes economy into account.
The invention is based on the basic idea of adapting the existing training ammunition to the fire control computer instead of changing the fire control computer, as has been the approach until now. In this regard, it is necessary to take into consideration the complex interaction between the temperature behavior of the ammunition from −15° C. to 35° C., and the trajectory.
The adaptation is carried out by increasing the diameter of the flare while the length of the tail piece is kept constant and also possibly providing the training ammunition with a different propellant charge powder. Amazingly, it was found in practice that a complex adaptation to the temperature and trajectory behavior is achieved in this way, and only a trajectory error (at −15° C. to 35° C.) of less than 0.1 is possible. An “I” propellant charge powder is used as the new propellant charge powder instead of a simple propellant charge powder.
The invention is explained in greater detail below with reference to the specific embodiment illustrated in the drawings.
a shows a tail piece.
The tail piece 2 illustrated here, which has a flare of, for example, 78 mm, is replaced by a tail piece 2.1 (
Although the present invention has been described in relation to particular embodiments thereof, many other variations and modifications and other uses will become apparent to those skilled in the art. It is preferred, therefore, that the present invention be limited but by the specific disclosure herein, but only by the appended claims
Number | Date | Country | |
---|---|---|---|
60790712 | Apr 2006 | US |