Abstract:
A propellant casing assembly for an electrothermic projectile firing device has a casing and an electrically energizable coil disposed in the casing. The coil vaporizes at a predetermined current intensity and generates at least one part of propellant gases for accelerating a projectile.

Description:
This application is a continuation of application Ser. No. 07/351,120, filed May 12, 1989 now abandoned. 
    
    
     BACKGROUND OF THE INVENTION 
     This invention relates to a propellant casing assembly for an electrothermic firing device for the acceleration of projectiles. 
     As disclosed, for example, in German Offenlegungsschrift (non-examined published application) U.S. Pat. No. 3,613,259, known firing devices whose operation is based on the electrothermic principle utilize the conversion of electromagnetic energy into thermal energy. It is a disadvantage of known electrothermic firing devices that the inductive storage elements for the energization are situated externally of the firing device and thus have an additional spatial requirement. It is a further disadvantage that for the charging of the inductive storage elements current intensities up to several hundreds of kiloamperes are needed which can be generated only by special energy sources such as homopolar generators or large condenser batteries. It is a further drawback that during the slow charging process of the storage elements, a substantial amount of energy is dissipated due to ohmic resistances. 
     SUMMARY OF THE INVENTION 
     It is an object of the invention to provide an improved casing assembly of the above-outlined type in which inductive storage elements can be disposed in a place-saving manner and which ensures that during charging of the storage elements energy losses are significantly reduced. 
     This object and others to become apparent as the specification progresses, are accomplished by the invention, according to which, briefly stated, in the casing a coil is disposed which, at a given current intensity vaporizes and thus constitutes entirely, or in part, the gas that propels the projectile. 
     Thus, according to the invention, the inductive storage element is situated within the casing proper. Upon completion of the supply of electromagnetic energy, the coil vaporizes and thus produces at least one part of the propellant gas which accelerates the projectile and further, the magnetic energy stored in the coil volume may be utilized for additionally heating the gas. 
    
    
     BRIEF DESCRIPTION OF THE DRAWING 
     FIGS. 1, 2 and 3 are axial sectional views of the breech part of a gun incorporating a preferred embodiment of the invention, illustrating three different operational phases. 
     FIG. 4 is a view similar to FIG. 1, illustrating one of the compounds as being of a different material. 
    
    
     DESCRIPTION OF THE PREFERRED EMBODIMENT 
     Turning to FIG. 1, there is illustrated therein the breech portion 10 of a gun barrel accommodating a propellant casing assembly 20 and the projectile 24. Current supply to the casing assembly is effected by a current supply device 30. The gun is closed with an end plate 11 and has a barrel bore 12. 
     The casing assembly 20 comprises a container or casing proper 21 made of steel, fiberglass-reinforced synthetic material (as shown in FIG. 4) or other high-strength substance, an insulating jacket 22 and a coil 23. The latter is formed of an insulated conductor made, for example, of aluminum, lithium or graphite. The remaining volume of the casing assembly 20 is filled with an appropriate propellant 25. Such propellant is of a low molecular weight material such as methanol, lithium hydride, lithium, methane, water or coal dust. The casing assembly 20, together with the projectile 24 attached thereto is inserted into the barrel 10 and is mechanically immobilized by the rear closure plate 11. 
     The current supply device 30 which is essentially formed of the current source 31 proper and a switch 32, is electrically directly connected by a conductor 40 with one end of the coil 23. The circuit is completed by a conductor 41 which connects the other end of the coil 23 to the current source 31 via the casing 21 and the barrel 10. 
     The inductivity of the coil 23 and thus its geometrical dimensions and number of turns are so designed that it can be charged to the desired magnetic energy by means of the maximum producible current from the primary energy source 31. The diameter of the coil turns is selected such that the turns vaporize as the maximum current intensity is reached as illustrated in FIG. 2. Thereupon, for maintaining the magnetic flux, the sum current of all coil turns continue to flow through the plasma thus generated. The magnetic energy which has been stored within the volume of the vaporizing coil is, in the ohmic resistance of the plasma converted to heat whereby the propellant material 25 (if present) is heated and converted into plasma. By virtue of the thermal pressure of the propellant gases generated in this manner, the projectile 24 is accelerated. 
     FIG. 3 depicts the barrel at a moment when the projectile 24 has been expelled from the casing assembly 21 but is still situated within the gun barrel 10 and the coil 23 has already evaporated. The container 21 and the insulating jacket 22 remain in the breech and must be removed before insertion of a new ammunition. 
     It will be understood that the above description of the present invention is susceptible to various modifications, changes and adaptations, and the same are intended to be comprehended within the meaning and range of equivalents of the appended claims.