Abstract:
Disclosed are a tungsten material for a penetrating splinter shell and forming method thereof enabling a penetrator to perforate a hard target on high-speed impact as well as having the following splinter cause a severe damage on an inner component by changing a breakage characteristic of the material into brittle fracture from ductile fracture in a manner that a mechanical characteristic of the material is adjusted by controlling a sintering condition and a composition ratio of a tungsten heavy alloy material having Mo added thereto. The present invention includes the steps of mixing 90˜95 wt % W powder, 3.0˜8.0 wt % Mo powder, 0.5˜3.0 wt % Ni powder, and 1.0˜4.0 wt % Fe powder with each other, molding the mixed powders, and sintering the molded powders.

Description:
[0001]    This application claims the benefit of the Korean Application No. P2002-40994 filed on Jul. 13, 2002, which is hereby incorporated by reference.  
         BACKGROUND OF THE INVENTION  
         [0002]    1. Field of the Invention  
           [0003]    The present invention relates to a tungsten heavy alloy applied to a penetrator material of a penetrating splinter shell, and more particularly, to a tungsten material for a penetrating splinter shell and forming method thereof enabling a penetrator to perforate a hard target on high-speed impact as well as having the following splinter cause a severe damage on an inner component by changing a breakage characteristic of the material into brittle fracture from ductile fracture in a manner that a mechanical characteristic of the material is adjusted by controlling a sintering condition and a composition ratio of a tungsten heavy alloy material having Mo added thereto.  
           [0004]    2. Discussion of the Related Art  
           [0005]    [0005]FIG. 1 illustrates a picture of a typical microstructure(compositional mode of SEM) of 90W-7Ni-3Fe tungsten heavy alloy according to a related art.  
           [0006]    Referring to FIG. 1, circular grains are tungsten of body-centered cubic(BCC) unit cells and a portion, which surrounds the circular grains and in which solid solution of the tungsten is contained in part, is a matrix of Ni—Co—Fe—W alloy of face-centered cubic(FCC) unit cells.  
           [0007]    The material is a kind of composite constructed with a tungsten particle having a hard property and the matrix having a soft property.  
           [0008]    Meanwhile, the material is prepared by liquid phase sintering. The prepared pellet is maintained at 1,000˜1,300° C. for a predetermined time(2˜10 hours), a series of water quenching is carried out on the pellet repeatedly, a cold rolling process is carried thereon, and the pellet is then aged.  
           [0009]    The pellet prepared by the above method is widely used as a penetrator material of a kinetic energy projectile as well as is applied to other civilian industry fields of weight balance, radiation shield, processing tool, and the like.  
           [0010]    Depleted uranium(hereinafter abbreviated DU) is currently used as a material of an armored plate breaking penetrator as well as the tungsten heavy alloy material.  
           [0011]    It is known that material physical properties of DU is superior to those of tungsten heavy alloy as well as that penetration performance of DU is superior to that of tungsten heavy alloy approximately 10%. The reason why the penetrating performance of DU is superior to that of tungsten heavy alloy is that a behavior of high-speed transformation of DU is different from that of tungsten heavy alloy. A difference between the high-speed transformation behaviors of the two materials is shown in FIG. 2A and FIG. 2B.  
           [0012]    Namely, tungsten heavy alloy, as shown in FIG. 2B, has severe transformation on penetration so that a cusp of the penetrator is changed into a mushroom shape to increase a diameter of the penetrator. Hence, a penetration resistance increases to reduce the penetrating performance. On the other hand, DU, as shown in FIG. 2A, develops so-called self-sharpening that causes a local fracture easily due to adiabatic shear bend at an edge of the cusp of the penetrator. Hence, a diameter of the penetrator of DU becomes smaller than that of tungsten heavy alloy so that a penetration resistance of DU is lowered than that of tungsten heavy alloy. Therefore, the penetrating performance of DU is relatively increased.  
           [0013]    There are several disadvantages to using DU, such as hydrogen brittleness, corrosion, environmental pollution, related medical illness, and the like. Therefore, notwithstanding that DU is superior to tungsten heavy alloy in penetrating power, the latter is on the balance more suitably useable.  
           [0014]    Specifically, environmental pollution and badness for human healthcare are fatal so that there are many limitations on use of DU.  
           [0015]    Military arms are variously developed lately to make use of the tungsten heavy alloy material for the kinetic energy projectile as attacking arms systems for missile defense, anti-ship, and anti-craft in Navy. Specifically, a penetrating splinter shell having multi-functions of splinter diffusion penetration and incendiary effect is badly demanded.  
           [0016]    Meanwhile, unlike the penetrating tool of target penetration by self-sharpening of the penetrator itself, a W—Cu material is known well for the target penetration by splinter diffusion. Yet, when considering the relative correlation of tensile strength and compression breakdown strength of the W—Cu material, is to apparent that the tensile strength is, relatively, too high. Hence, the W—Cu material fails to be superior to that of the present invention in the splinter-diffusion penetrating performance.  
         SUMMARY OF THE INVENTION  
         [0017]    Accordingly, the present invention is directed to a diffusing-splinter penetration type tungsten heavy alloy penetrator material that substantially obviates one or more problems due to limitations and disadvantages of the related art.  
           [0018]    An object of the present invention is to provide a diffusing-splinter penetration type tungsten heavy alloy penetrator material enabling to penetrate a target not by self-sharpening of a penetrator itself but by splinter diffusion.  
           [0019]    Additional advantages, objects, and features of the invention will be set forth in part in the description which follows and in part will become apparent to those having ordinary skill in the art upon examination of the following or may be learned from practice of the invention. The objectives and other advantages of the invention may be realized and attained by the structure particularly pointed out in the written description and claims hereof as well as the appended drawings.  
           [0020]    To achieve these objects and other advantages and in accordance with the purpose of the invention, as embodied and broadly described herein, a diffusing-splinter penetration type tungsten heavy alloy penetrator material according to the present invention includes 90˜95 wt % W powder, 3.0˜8.0 wt % Mo powder, 0.5˜3.0 wt % Ni powder, and 1.0˜4.0 wt % Fe powder.  
           [0021]    In another aspect of the present invention, a method of forming a diffusing-splinter penetration type tungsten heavy alloy penetrator material includes the steps of mixing 90˜95 wt % W powder, 3.0˜8.0 wt % Mo powder, 0.5˜3.0 wt % Ni powder, and 1.0˜4.0 wt % Fe powder with each other, molding the mixed powders, and sintering the molded powders.  
           [0022]    Preferably, the molding step is carried out by Cold Iso Press.  
           [0023]    Preferably, the sintering step is carried out for 2˜5 hours at 1,350˜1,450° C.  
           [0024]    Preferably, the sintering is carried out at an ambience of none-oxidation or a reducing ambience of hydrogen gas.  
           [0025]    The present invention is characterized in that a mechanical characteristic is controlled by an intermetallic compound produced by adjusting an alloy ratio by adding Mo to a tungsten heavy alloy composition and by controlling a sintering condition.  
           [0026]    Therefore, the present invention enables to provide a heavy alloy material for a splinter shell suitable for penetrating the target on high-speed impact and causing a severe damage on an inner component by changing a breakage characteristic of the material into brittle fracture from ductile fracture  
           [0027]    It is to be understood that both the foregoing general description and the following detailed description of the present invention are exemplary and explanatory and are intended to provide further explanation of the invention as claimed.  
       
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS  
       [0028]    The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the invention and together with the description serve to explain the principle of the invention. In the drawings:  
         [0029]    [0029]FIG. 1 illustrates a picture of a micro structure(compositional mode of SEM) of 90W-7Ni-3Fe tungsten heavy alloy according to a related art;  
         [0030]    [0030]FIG. 2A illustrates a diagram of a transformation behavior generated from a cusp of a uranium(DU) penetrator on high-speed impact;  
         [0031]    [0031]FIG. 2B illustrates a diagram of a transformation behavior generated from a cusp of a tungsten heavy alloy penetrator on high-speed impact;  
         [0032]    [0032]FIG. 3A illustrates microscopic pictures of microstructures of a tungsten heavy alloy material having a splinter diffusion characteristic according to a disclosed W—Cu material;  
         [0033]    [0033]FIG. 3B illustrates microscopic pictures of microstructures of a tungsten heavy alloy material having a splinter diffusion characteristic according to a material of the present invention;  
         [0034]    [0034]FIG. 4 illustrates a graph of forming an intermetallic compound according to a sintering temperature and a cooling condition of a tungsten heavy alloy material;  
         [0035]    [0035]FIG. 5 illustrates a stress-strain graph of a compression strength test for an alloy ratio variation of each sample according to the present invention;  
         [0036]    [0036]FIG. 6A illustrates a picture of a fracture pattern of sample a(93.8W-2.5Ni-3.7Fe) in FIG. 5;  
         [0037]    [0037]FIG. 6B illustrates a picture of a fracture pattern of sample b(93.7W-1.5Ni-1.87Fe-3.0Mo), sample c(93.1W-1.1Ni-1.3Fe-4.5Mo), and sample d(92.0W-0.5Ni-1.0Fe-6.5Mo)in FIG. 5;  
         [0038]    [0038]FIG. 6C illustrates a picture of a fracture pattern of a disclosed sample e(W—Cu) in FIG. 5;  
         [0039]    [0039]FIG. 7 illustrates a stress-strain graph of a compression strength test for the sample c(93.1W-1.1Ni-1.3Fe-4.5Mo) according to each sintering temperature;  
         [0040]    [0040]FIG. 8A illustrates a picture of a fracture pattern of the sample c in compression strength test according to a sintering temperature(1,390° C.);  
         [0041]    [0041]FIG. 8B illustrates a picture of a fracture pattern of the sample c in compression strength test according to a sintering temperature(1,410° C.);  
         [0042]    [0042]FIG. 8C illustrates a picture of a fracture pattern of the sample c in compression strength test according to sintering temperatures(1,390° C., 1,450° C.);  
         [0043]    [0043]FIG. 9 illustrates a stress-strain graph of a compression strength test for the sample c(93.1W-1.1Ni-1.3Fe-4.5Mo) according to each sintering time;  
         [0044]    [0044]FIG. 10A illustrates a picture of a fracture pattern of the sample c at the sintering temperature of 1,410° C.) in compression strength test according to the sintering time(2 hours);  
         [0045]    [0045]FIG. 10B illustrates a picture of a fracture pattern of the sample c at the sintering temperature of 1,410° C.) in compression strength test according to the sintering time(3.5 hours, 5 hours);  
         [0046]    [0046]FIG. 11A illustrates a picture of splinter pieces after compression test of a disclosed material(W—Cu);  
         [0047]    [0047]FIG. 11B illustrates a picture of splinter pieces after compression test of a material(93.1W-1.1Ni-1.3Fe-4.5Mo) of the present invention;  
         [0048]    [0048]FIG. 12A illustrates a SEM picture of a splinter after compression test of the sample b(93.7W-1.5Ni-1.8Fe-3.0Mo);  
         [0049]    [0049]FIG. 12B illustrates a SEM picture of a splinter after compression test of the sample c(93.1W-1.1Ni-1.3Fe-4.5Mo);  
         [0050]    [0050]FIG. 13 illustrates a diagram of armored target arrangement of a penetrating splinter shell;  
         [0051]    [0051]FIG. 14A illustrates a picture of a penetrated target by a disclosed material(W—Cu); and  
         [0052]    [0052]FIG. 14B illustrates a picture of a penetrated target by the sample c of the present invention. 
     
    
     DETAILED DESCRIPTION OF THE INVENTION  
       [0053]    Reference will now be made in detail to the preferred embodiments of the present invention, examples of which are illustrated in the accompanying drawings. Wherever possible, the same reference numbers will be used throughout the drawings to refer to the same or like parts.  
         [0054]    A tungsten heavy alloy material according to the present invention has a Mo content of 3.0˜8.0 wt % to increase hardness and compression breakdown strength but to decrease tensile strength. This is because Mo becomes an intruder into tungsten grains to increase the compression breakdown strength by causing lots of transformation of the tungsten grains.  
         [0055]    Moreover, as the splinter becomes a straight line shape by Mo addition, the tensile strength becomes smaller than the compression breakdown strength, thereby possibly causing a sever damage on a an inner component for breakage.  
         [0056]    This is a phenomenon occurring in a manner that a dislocation generated from compression transformation of Mo as an intrusive element having intruding into the tungsten grains is coupled with a tungsten gain. It is known that a new dislocation is generated from a stress-focused point when the dislocation is released by high compression stress or is bound strongly.  
         [0057]    A sintering temperature to acquire a material according to the present invention is 1,300˜1,500° C., and preferably, 1350˜1,450° C. If the temperature is raised higher, the compression breakdown strength is reduced but the tensile strength is increased. Hence, a step-like fracture pattern is formed to reduce the breaking characteristic. This means that an intermetallic compound tends to be formed less if cooling is carried out at high temperature instead of low temperature. In this case, brittleness of the material appears less. Moreover, if the sintering temperature is too low, the fracture pattern of the material fails to be straight.  
         [0058]    In aspect of the sintering time, the longer the sintering time gets at the same temperature, the higher the tenacity of the material gets. The shorter the time becomes, the higher the compression breakdown strength becomes but the less the tensile strength becomes. Hence, the sintering time of the present invention is preferably 2˜5 hours.  
         [0059]    The tungsten heavy alloy penetrator material according to the present invention, on which sintering is carried out on the above-explained condition, has such mechanical characteristics as 30˜36 of hardness(HRC), 40˜75 kg/cm 2 (preferably, 47˜67 kg/cm 2 ) of tensile strength, and 80˜100 kg/cm 2  (preferably, 85˜95 kg/cm 2 ) of compression breakdown strength.  
         [0060]    First Embodiment  
         [0061]    In accordance with the composition of Table 1, four species of sample (a) 93.8W-2.5Ni-3.7Fe, sample (b) 93.7W-1.5Ni-1.8Fe-3.0Mo, sample (c) 93.1W-1.1Ni-1.3Fe-4.5Mo, and sample (d) 92.0W-0.5Ni-1.0Fe-6.5M0 are mixed with other. After that, a form having a diameter of 25 mm and a length of 350 mm is prepared by Cold Iso Press. And, the form is sintered at a reducing gas ambience of hydrogen using a Pusher type consecutive sintering furnace. A tensile sample is prepared from the produced material according to ASTM-E8M FIG. 20 and a compression sample of Φ10 mm×L10 mm is prepared. And, physical property tests are carried out on both of the prepared samples at a test speed of 0.5 mm/min. The test results are shown in Table 1.  
                                                                                                                   TABLE 1                           Physical property change according to       composition ratio of raw material powder                class. cl.                Compression test                Tensile       Compression                           wt %   Strength   Hard.   Breakdown   Fraction   Splinter   S-S   Density       Comp. (wt %)   (kg/mm 2 )   (H R C)   (kg/mm 2 )   pattern   count   curve   (g/cc)   Ref.                    (a)   93.8W-   84   34.0   77       10       17.72   Sintering           2.5N-                               for 2           3.7Fe-                               hours at           0.0Mo                               max.       (b)   93.7W-   58   34.5   88       8       17.80   1,410° C.           1.5Ni-           1.8Fe-           3.0Mo       (c)   93.1W-   53   34.5   90   12   17.88           1.1Ni-           1.3Fe-           4.5Mo       (d)   92.0W-   43   36.0   105   13   17.55           0.5Ni-           1.0Fe-           6.5Mo                  
 
         [0062]    [0062]FIG. 3B illustrates microscopic pictures of microstructures of sample c having a splinter diffusion characteristic in Table 1.  
         [0063]    Referring to FIG. 3B, as the Mo contents increases like in Table 1, hardness and compression breakdown strength increase but tensile strength decreases. Since Mo as an intrusive type resides in tungsten(W) grains, transformation is greatly given to the tungsten grains to increase the compression breakdown. Moreover, tensile strength increases due to the incremental contents of Ni and Fe as binding metals since the strength and ductility increase due to the formation of all-ratio solid solution.  
         [0064]    [0064]FIG. 12A illustrates a SEM picture of a splinter after compression test of the sample b(93.7W-1.5Ni-1.8Fe-3.0Mo) and FIG.  12 B illustrates a SEM picture of a splinter after compression test of the sample c(93.1W-1.1Ni-1.3Fe-4.5Mo).  
         [0065]    Referring to FIG. 12A and FIG. 12B, as the Mo content increases, so does a grain size of tungsten, thereby increasing the transformation resistance. Moreover, in aspect of splinters in the compression test, shear(intercrystalline) fracture occurs on breakage since the sample a has the step-like tensile strength relatively higher than the compression breakdown strength. And, cleavage fracture occurs in the sample b, c, or d having a straight-lined tensile strength relatively smaller than the compression breakdown strength.  
         [0066]    [0066]FIG. 5 illustrates a stress-strain graph of a compression strength test for alloy ratio variation in Table 1.  
         [0067]    Referring to FIG. 5, the up and down breakdown phenomenon shows up in the samples b, c, and d. Such a phenomenon occurs in a manner that a dislocation generated from compression transformation of Mo as an intrusive element having intruding into the tungsten grains is coupled with a tungsten gain. It is known that a new dislocation is generated from a stress-focused point when the dislocation is released by high compression stress or is bound strongly.  
         [0068]    A splinter count of the material having a breakdown point in the stress-strain graph is greater than that having no breakdown point, and the splinters of the material having the breakdown point are similar to each other in size. Besides, a fracture pattern of the material having the breakdown point is a straight line. Hence, numerous splinters uniform in size are formed by the penetration test, whereby a penetrating diameter is increased greatly.  
         [0069]    [0069]FIG. 6A illustrates a picture of a fracture pattern of sample a(93.8W-2.5Ni-3.7Fe) in FIG. 5, FIG. 6B illustrates a picture of a fracture pattern of sample b(93.7W-1.5Ni-1.87Fe-3.0Mo), sample c(93.1W-1.1Ni-1.3Fe-4.5Mo), and sample d(92.0W-0.5Ni-1.0Fe-6.5Mo) in FIG. 5, and FIG. 6C illustrates a picture of a fracture pattern of a disclosed sample e(W—Cu) in FIG. 5.  
         [0070]    Second Embodiment  
         [0071]    A physical property change of a form of the sample c in the first embodiment of the present invention according to variation of sintering temperature is measured, and its results are shown in Table 2.  
         [0072]    [Table 2] Physical property change according to sintering temperature  
                                                                         TABLE 2                           Physical property change according to sintering temperature                sintering cl. temperature (mas. ° C.)                Compression test                Tensile       Compression                               strength       Breakdown   Fracture   Splinter   S-S   Density           wt %   (kg/mm 2     Hard. (H R C)   (kg/mm 2 )   pattern   count   curve   (g/cc)   Ref.               1,390   41   35.5   97       Perfect       17.58   Maintained                           micro           2 hours at                           splinters           max. temp.       1,410   53   34.5   90       12       17.68       1,430   63   32.6   76       10       17.69       1,450   74   31.6   68       8       17.71                  
 
         [0073]    And, a stress-strain graph of a compression strength test for the sample c(93.1W-1.1Ni-1.3Fe-4.5Mo) according to each sintering temperature is shown in FIG. 7.  
         [0074]    [0074]FIG. 8A illustrates a picture of a fracture pattern of the sample c in compression strength test according to a sintering temperature of 1,390° C., FIG. 8B illustrates a picture of a fracture pattern of the sample c in compression strength test according to a sintering temperature of 1,410° C., and FIG. 8C illustrates a picture of a fracture pattern of the sample c in compression strength test according to sintering temperature of 1,450° C.  
         [0075]    An effect that the sintering temperature affects the material characteristic is shown in Table 2. The stress-strain graph becomes curved as the temperature is higher on the same condition, a fracture pattern becomes step-like, a compression breakdown strength vale decreases, and a tensile strength value increases.  
         [0076]    The breakage characteristics of the material differ from each other since the product amount of the intermetallic compound in the material varies according to a setup range of the sintering temperature. Namely, the intermetallic compound of the material is generated in the course of cooling. And, a generation section of an intermetallic compound according to a sintering temperature and a cooling condition of a tungsten heavy alloy material is shown in FIG. 4. Referring to FIG. 4, a generation time (c) in the course of cooling at high temperature(1,450° C.) is much shorter than a time (a) of generating intermetallic compound in the course of cooling at 1,410° C.  
         [0077]    As shown in the test result, when the sintering temperature gets higher, the tensile strength increases but the compression breakdown strength decreases. This means that the intermetallic compound tends to be produced less if cooling is carried out at the high temperature instead of the low temperature. In this case, the brittleness shows up less. However, if the sintering temperature is too low, the fracture pattern of the material fails to be straight but becomes totally broken. Hence, it is verified that 1,410° C. of the sintering temperature is minimum.  
         [0078]    Third Embodiment  
         [0079]    A physical property change of a form of the sample c in the first embodiment of the present invention according to variation of sintering time is measured, and its result is shown in Table 3.  
                                                                                                               TABLE 3                           Physical property change according to       sintering time                sintering cl. time at max. temp.                Compression test                Tensile       Compression                           wt %   strength       Breakdown   Fracture   Splinter   S-S   Density           (hour)   (kg/mm 2 )   Hard. (H R C)   (kg/mm 2 )   pattern   count   curve   (g/cc)   Ref.                    2.0   53   34.5   90       12       17.68   Max.       3.5   69   32.4   78       10       17.65   sintering       5.0   74   31.6   69       8       17.68   temp.                                       1,410° C.                  
 
         [0080]    [0080]FIG. 9 illustrates a stress-strain graph of a compression strength test for the sample c(93.1W-1.1Ni-1.3Fe-4.5Mo) according to each sintering time, FIG. 10A illustrates a picture of a fracture pattern of the sample c at the sintering temperature of 1,410° C.) in compression strength test according to the sintering time(2 hours), and FIG. 10B illustrates a picture of a fracture pattern of the sample c at the sintering temperature of 1,410° C.) in compression strength test according to the sintering time(3.5 hours, 5 hours).  
         [0081]    Table 3 verifies that the material characteristics are affected by the variation of the sintering time. As the sintering time gets longer at the same temperature, the tenacity becomes higher. Namely, a tensile strength value increases but a compression breakdown strength value decreases. Specifically, a stress-strain graph is curved.  
         [0082]    In the second and third embodiments of the present invention, the compression breakdown strength increases if the sintering temperature or time decreases.  
         [0083]    [0083]FIG. 11A illustrates a picture of splinter pieces after compression test of a disclosed material(W—Cu) and FIG. 11B illustrates a picture of splinter pieces after compression test of a material(93.1W-1.1Ni-1.3Fe-4.5Mo) of the present invention.  
         [0084]    The material according to the present invention demanded in view of function prefers to be low in tensile strength. Yet, the material should be stable against the pressure of propellant inside a barrel on fire. Properly, The tensile strength is at least 47.0 kg/mm 2  and the compression breakdown strength is about 90 kg/mm 2 . It is confirmed that the optimal conditions of the sintering temperature and time are max. 1,410° C. and approximately two hours, respectively.  
         [0085]    Fourth Embodiment  
         [0086]    A test of splinter-diffusing penetration performance is carried out on a tungsten heavy alloy according to the present invention. When an optimal composition ratio of a raw material powder and the structure and physical/mechanical properties of a pellet in the tungsten heavy alloy according to the embodiment of the present invention are examined, it is judged that the sample c meets the requirements of the demanded penetrator material characteristics. Hence, comparison tests of penetration are carried out on the sample c and the disclosed penetrator material of W—Cu. And, the test results are shown in Table 4.  
                                                     TABLE 4                       Penetrator   Sample   Penetration            material   count (RDS)   diameter (Φ, mm)   Ref.                                Pen         ator   10   N         .   S         t   L         g           material       2   a         s   a         s                   3   110   110                   4   100   110                   5   80   135                   6   130   150                   7   80   80                   8   100   120                   9   120   120                   10   100   110                   Average   98.0   114.5                   1   150   150                   2   90   170                   3   100   120                   4   100   150                   5   100   120                   6   110   140                   7   180   200                   8   120   20                   9   100   110                   10   90   100                   Average   114.0   138.0                      
 
         [0087]    In the test results of penetration performance, a penetration diameter of a liquid phase sintering product of W—Ni—FE—Mo includes short axis Φ114 mm˜long axis Φ138 mm in average an the disclosed W—Cu material includes short axis Φ98 mm˜long axis Φ114.5 mm.  
         [0088]    [0088]FIG. 13 illustrates a diagram of armored target arrangement of a penetrating splinter shell, FIG. 14A illustrates a picture of a penetrated target by a disclosed material(W—Cu), and FIG. 14B illustrates a picture of a penetrated target by the sample c of the present invention.  
         [0089]    Accordingly, the present invention adjusts the overall composition ratio properly by adding Mo powder to tungsten heavy alloy powder and controls the sintering conditions, thereby enabling to change the breakage characteristics of the material into brittle fracture from ductile fracture in accordance with the amount of the product of the intermetallic compound. Therefore, the present invention provides, for a splinte shell on penetrator material that facilitates splinter diffusing penetration on the target at high speed impact.  
         [0090]    It will be apparent to those skilled in the art that various modifications and variations can be made in the present invention. Thus, it is intended that the present invention covers the modifications and variations of this invention provided they come within the scope of the appended claims and their equivalents.