[0001] This invention relates to an explosive small arms projectile, that is a projectile
filled with an explosive charge.
[0002] In this specification, the subject of the invention will be referred to as a "projectile",
although strictly speaking a bullet or missile is a projectile only while in flight.
The term "projectile"is, however, commonly used to denote the bullet or missile while
at rest or whilst in flight, and will be so used in the specification.
[0003] Such projectiles are used mainly in combating crime, particularly international terrorism,
where, on an aircraft, for instance, an explosive projectile may be used to take out
a target from within a group of innocent bystanders. Complete penetration of the target
may result in harm to the bystanders and it is therefore an object of explosive projectiles
to eliminate or at least minimize, total penetration of the target while maximizing
the shock from the projectile within the target.
[0004] The objective of the inclusion of high explosives (taken to include primary explosives
such as Mercury Fulminate or Lead Azide, and secondary explosives such as pentaerythritol
tetranitrate (PETN) or mannitol hexanitrate) in small arms projectiles may be conceived
of- primarily as enhancing the shocking effect of the projectile in the target and
the prevention of the projectile's penetration to any point beyond the intended objective
where the projectile may cause unintended injury or damage.
[0005] Known small arms projectiles are commonly constructed with a jacket of a relatively
light weight yet strong material such as steel and gilding metal, and a core of a
relatively heavy material which may be partly filled with explosive.
[0006] The jacket of a conventional explosive small arms projectile is typically of a wear/resistant
material such as steel which is gilded or clad with gilding metal, the steel providing
mechanical strength to withstand the pressures and high temperatures resulting from
burning propellants and the gilding metal being provided for the purpose cf reducing
friction. On known explosive small arms projectiles, the steel jacket is normally
thin and largely non-structural, the functions thereof being containment of the lead
core more than maintaining the integrity of the projectile on impact. This results
in limited penetration of a target with the result that light armor is often sufficient
to prevent penetration.
[0007] In prior art small arms explosive projectiles, the explosive is normally carried
within a narrow central bore formed in the lead core. The explosive may comprise a
simple explosive train of an impact sensitive primary explosive, such as, for example,
Lead Azide, or a more complicated version comprising three stages; a first stage constituted
by an impact sensitive mechanism, an initiating or primary explosive such as, for
'example, Mercury fulminate as second staga;terminating in a third stage of a secondary
high explosive such as (PETN). Some designs have employed, as the high explosive,
a poly- basic glycerol trinitrate/pyrocellulose smokeless propellant powder which
is a combustible solid and an explosive, and which'burns to detonation', but without
optimal explosive utilization.
[0008] The deficiencies in the effect of prior art explosive small arms projectiles lie
in failure to effect and maintain optimal required ballistic rotational stabilization,
owing to limitations of conventional explosive projectile mass and mass distribution,
thus leading to deficiencies in long range performance and accuracy; deficiencies
in penetration owing to diminished mass; and perhaps most significantly, deficiencies
in the propogation of the secondary high explosive shock wave within the necessarily
narrow '(5 mm diameter (3/16") in a .38 caliber projectile) conventional explosive
column. This last deficiency results from the relatively restricted diameter of the
explosive which is constrained to function in a high velocity rotational mode within
a lead sheath of low strength which is subject to plastic deformation on impact. An
efficient 3-stage .38 caliber projectile containing a 5mm diameter PETN explosive
column initiated in flight may suffer non-detonation of 10-14% of its PETN column
when detonation occurs within an airfilled space.
[0009] It is an object of this invention to provide an explosive small arms projectile with
the mass thereof re-distributed to the periphery so as to be subject to investment
with a higher rotational stabilizing energy than was possible with prior art projectiles,
resulting in improved accuracy upon chosen targets at an increased range. This includes
a re-distribution of the projectile mass away from the rotational axis of the projectile
whereby the in-flight ballistic rotational stabilizing force and energy of the projectile
is improved with respect to known high explosive projectiles of similar total mass
and configuration.
[0010] It is a further object of this invention to provide an explosive small arms projectile
in which the explosive column diameter is increased as a means of reducing explosive
non-utilization. It is yet a further object of this invention to provide an explosive
small arms projectile, the explosive containing envelope of which shows an increase
in tensile and inertial characteristics over the conventional lead or copper or steel
jacketed lead projectiles.
[0011] These results are obtained by the use in an explosive small arms projectile, of a
jacketing material with a specific gravity greater than 13 or a density in excess
of 13g.cm , the preferred jacket material comprising tantalum or Tantalum-Tungsten
alloys, the densities of which approximate 16.6 to 16.9 g.cm-
3, the object being to provide a projectile the jacket of which has a mass equal to
the entire conventional explosive or other projectile.
[0012] The jacket is of metal or an aggregate. By "aggregate" is included alloys, mixtures
or compounds of metals.
[0013] The metal or aggregate of the jacket may be Tantalum or a Tantalum/Tungsten alloy,
or may include Tantalum or a Tantalum/Tungsten alloy as principal component.
[0014] Alternatively the metal or aggregate of the jacket may be chosen from amongst the
elements Hafnium, Uranium, Rhenium, Osmium, Platinum, Iridium or Gold, or alloys,
mixtures or compounds of the said elements, which alloys, mixtures or compounds may
include Tantalum or Tungsten or both.
[0015] As with prior art projectiles the projectiles of the invention may be coated or gilded
or, alternatively, the jacket may be metal-plated or metal clad on one or both sides.
[0016] The invention is further described with reference to the accompanying drawings in
which:
Figure 1 is a section through a prior art explosive projectile; and
Figure 2 is a section through an explosive projectile according to the invention.
[0017] The projectile 10 shown in Figure 1 comprises a relatively thin steel jacket 12 with
gilding metal 14 and 16 plated on both the inside and outside thereof. The projectile
10 is provided with a lead core 18 formed with a central bore 20 which serves as a
receptacle for the explosive.
[0018] The explosive may be loaded in any one of a number of ways, but for the sake of clarity
is shown as comprising a charge of explosive powder 22, a commercially available small
arms percussion primer 24 and a closure of resin 26.
[0019] As already explained, the purpose of the jacket is to withstand the pressures and
high temperatures resulting from the burning propellants and to withstand the frictional
forces between the lands and grooves of the barrel, of the firing weapon and the accelerating
projectile. The lead core 18 functions to increase the mass of the projectile whereby
the momentum of the projectile may be increased. The primer 24 is intended to detonate
the explosive 22 on impact, but it will be appreciated that the projectile 10 will
have penetrated the target to a certain extent by the time detonation occurs due to
the velocity of the projectile.
[0020] The projectile shown in the drawing is enlarged for clarity and in a .38 caliber
projectile the central bore 20 will have a diameter of 5mm. A .38 caliber projectile
containing a three-stage explosive column, in which detonation is initiated in flight
has been found to suffer nom-detonation of 10-14% of its explosive column when detonation
occurs within an air-filled space. The reason for this is that the conventional explosive
projectile can sacrifice only a limited proportion of its total volume to explosive
content in order to retain the mass thereof thus leading to an explosive column of
relatively narrow diameter, in which the explosive shock wave front is propagated
inefficiently particularly under the high velocity rotational condition of actual
use.
[0021] As has also been mentioned, the thin steel jacket 12 performs a containment function
more than anything else and possesses sufficient mechanical strength merely to withstand
the frictional forces existing between the projectile and the lands and grooves of
the barrel during firing. The jacket is not possessed of the medhanical strength required
to maintain optimal integrity of the projectile when the projectile penetrates the
target.
[0022] The disadvantages of the projectile 10 described above are therefore firstly, the
sacrifice of a significant proportion of the mass, as much as 20% of the leaden mass,
to accommodate a certain amount of explosive, secondly, the use of a narrow diameter
explosive column, thirdly, the relatively limited tensile strength and unsatisfactory
inertial characteristics of the jacket or envelope and fourthly, the unsatisfactory
mass distribution thereof resulting in relatively low rotational stabilising energy
values compared to the projectile of the present invention. It will be seen that,
in a conventional small arms explosive projectile as described above, a compromise
must be struck between the core mass which is normally represented by the amount of
lead in the core and the diameter of the explosive column. It is not possible, with
conventional small arms explosive projectiles, to combine both the attributes of high
mass and a large amount of explosive or at least an explosive column of a larger diameter.
[0023] A solution of these deficiencies may be found in the projectile 100 of the invention
which is shown in Figure 3. The projectile 100 comprises a jacket 102 of a Tantalum/
Tungsten alloy (TaW) although other metals of suitably high specific gravity may be
used. Because of the high specific gravity of the jacket 102 no internal high density
core is required and the whole of the internal space can be filled with explosive.
A three-stage explosive column is shown comprising a commercially available small
arms percussion primer 104, a lead azide primary explosive layer 106, a secondary
high explosive layer of PETN 108, and a sealing cap of resin 110.
[0024] The eventual mass of the projectile 100 is arranged to be at least equivalent to
that of the projectile 10 described above. In projectiles of equivalent mass the provision
of the hεavy metal jacket 102 may not remedy entirely the mass lost in providing the
projectile 10 with the explosive core, but the diminished mass is at least distributed
more efficiently so as to render the mass of the projectile susceptible to investment
with a higher level of rotational stabilizing energy than is possible with the projectile
10.
[0025] It will be immediately evident that the explosive column has been increased in volume
by approximately 250% whereby explosive non-utilization is reduced from the 10-14%
non-utilization of the prior art projectiles to a point such that is is not readily
detectable and is assumed to be significantly below 1% if not effectively complete.
[0026] The tensile and inertial characteristics of the Tantalum/ Tungsten alloy jacket 102
are increased with respect to the prior art jackets to a point potentially approximating
the tensile characteristics of steel or alloy steel and with an improved inertial
characteristic approximating 46% in excess of a lead envelope (calculated on a density
basis of 16.6g.cm
-3 for TaW and 11.4g.cm
-3 for Pb so that (16.6/ 11.4) -1 = 0.46).
[0027] In addition the projectile mass is efficiently redistributed away from the rotational
axis of the projectile and closer to its periphery in contact with the bore of the
weapon so as to equal and exceed, in flight, the ballistic rotational stabilizing
force and energy present in conventional small arms high explosive projectiles of
similar total mass and configuration. This re-distribution and increased rotational
stabilizing force provides for improved accuracy at longer range.
[0028] These results can be confirmed by a rough comparison, based on calculation, of the
projectile of the invention with a prior art explosive projectile with reference to
two long-standing American military service weapons, namely, the US Model 1911 .45
ACP (Colt Automatic Pistol), firing a 230 grain (14.9g) projectile and the (30-06)
US Caliber 30 (MlA2 Ball) rifle firing a 150 grain (9.7g) projectile.

[0029] From the above table, it may be seen that, whereas the conventional small arms explosive
projectile is bracketed, in terms of muzzle energy, between the conventional non-explosive
bullet as fired from a pistol and a conventional non-explosive bullet as fired from
a rifle, an explosive pistol bullet according to the present invention is bracketed
between a conventional non-explosive projectile as fired from a rifle and a conventional
non-explosive projectile as fired from a big game-hunting rifle. It will, however,
be appreciated that the present invention provides, in a highly manoeuverable .45
Caliber hand-gun, muzzle energies 50% in excess of those provided by a heavy service
rifle such as the US Caliber .30 Ml, and nearly ten times that of the non-explosive
.45 Caliber ACP Projectile when both are compared by firing from an identical .45
Caliber Automatic Pistol.
[0030] The term "muzzle energy" is used here to denote the maximum theoretical energy the
projectile can deliver to the target. In instances where a non-explosive projectile
is retained in the target, thereby communicating the total energy thereof to the target,
the energy expended in the target will, discounting frictional and gravitational energy
loss, be more or less equal to the energy of the projectile at the muzzle of the weapon.
If the projectile penetrates the target, substantially less of the energy of the projectile
will be communicated to the target depending on the nature of the penetration;with
explosive projectiles, however, the projectile will, in virtually every case, transfer
all of its energy to the target.
[0031] In the prior art, explosive projectile 10 shown in Figure 1, any increase in jacket
thickness will have to be made at the expense of a decrease in the core mass leading
inevitably to a decrease in the total projectile mass. In the projectile 100 of the
present invention, the jacket 102 can, within certain limits, be increased to any
desired thickness to increase the tensile and mass characteristics of the jacket according
to specific requirements, for instance, to increase the penetrational ability of the
projectile. Preferably the mass of the projectileis largely concentrated in the jacket
which, to this end, is relatively thick. In this manner, within the space limited
small arms context, the twin functions of energy absorption by a heavy mass and the
jacket features of mechanical, structural and tensile strength, are condensed into
a single entity. In the past, the energy absorbing heavy mass was provided by the
lead core and structural integrity was provided, to a limited extent, by the steel
or copper jacket. The improved stability achieved by the projectile of the present
application, provides increased accuracy and this combined with the greater structural
strength of the jacket provides for better penetration of light armor. While the projectile
of the present invention is described above with specific reference to a hand gun
projectile, it is evidently adaptable to the entire range of small arms projectiles,
the term "small arms" being taken to indicate any weapon whether mounted or not, which
is portable.
1. An explosive small arms projectile (100) comprising a jacket (102) of metal or
an aggregate and an explosive charge (104, 106, 108) located therein, characterised
in that the metal or aggregate of the jacket (102) has a specific gravity greater
than 13.
2. A projectile according to claim 1, characterised in that the metal or aggregate
of the jacket is Tantalum or a Tantalum/Tungsten alloy or includes Tantalum or a Tantalum/Tungsten
alloy as principal component.
3. A projectile according to claim 1, characterised in that the metal or aggregate
of the jacket is chosen from amongst the elements Hafnium, Uranium, Rhenium, Osmium,
Platinum, Iridium or Gold, or alloys, mixtures of compounds may include Tantalum or
Tungsten or both.
4. A projectile according to any one of the preceding claims characterised in that
the mass of the projectile is largely concentrated in the jacket which, to this end,
is relatively thick.