U.S. patent application number 11/779568 was filed with the patent office on 2011-04-07 for warhead booster explosive lens.
This patent application is currently assigned to Raytheon Company. Invention is credited to E. RUSS ALTHOF, William R. Hawkins, Henri Y. Kim.
Application Number | 20110079162 11/779568 |
Document ID | / |
Family ID | 39721757 |
Filed Date | 2011-04-07 |
United States Patent
Application |
20110079162 |
Kind Code |
A1 |
ALTHOF; E. RUSS ; et
al. |
April 7, 2011 |
WARHEAD BOOSTER EXPLOSIVE LENS
Abstract
A cost-effective solution is proposed to improve explosive
transfer between booster and warhead that is compatible with the
existing base of general purpose warheads and flexible to work with
new warhead configurations. A booster lens is placed in the fuze
well that concentrates the pressure wave to penetrate the fuze well
with a peak pressure that exceeds the detonation threshold and
detonate the warhead explosive. The booster lens can be configured
to control the direction of the concentrated lobe to penetrate the
fuze well where the barriers are low.
Inventors: |
ALTHOF; E. RUSS; (Tucson,
AZ) ; Hawkins; William R.; (Abilene, TX) ;
Kim; Henri Y.; (Tucson, AZ) |
Assignee: |
Raytheon Company
|
Family ID: |
39721757 |
Appl. No.: |
11/779568 |
Filed: |
July 18, 2007 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
|
|
60823874 |
Aug 29, 2006 |
|
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|
Current U.S.
Class: |
102/275.9 |
Current CPC
Class: |
F42B 1/024 20130101;
F42B 3/10 20130101; F42B 3/22 20130101; F42C 19/0838 20130101 |
Class at
Publication: |
102/275.9 |
International
Class: |
F42C 19/08 20060101
F42C019/08; F42C 19/00 20060101 F42C019/00; F42C 19/02 20060101
F42C019/02 |
Claims
1. A munition, comprising: a warhead including a fuze well and a
warhead explosive around the fuze well; a booster including a
booster explosive placed inside the fuze well, said fuze well
providing a barrier between the booster explosive and warhead
explosive; a fuze behind the booster inside the fuze well that
detonates the booster explosive creating a pressure wave with a
peak pressure, said pressure wave having a forward axial component
and a radial component; and a booster lens having a surface, said
booster lens positioned in the fuze well to re-direct a portion of
the radial component of the pressure wave off of the lens surface
in the axial direction to concentrate the pressure wave into a lobe
in a predetermined direction with increased peak pressure to
penetrate the barrier provided by the fuze well and directly
detonate the warhead explosive approximately axially from the
booster.
2. The munition of claim 1, wherein the peak pressure of the
booster pressure wave does not exceed a pressure threshold to
detonate the warhead explosive, said increased peak pressure of the
lobe exceeding the pressure threshold to directly detonate the
warhead explosive.
3. (canceled)
4. (canceled)
5. (canceled)
6. (canceled)
7. (canceled)
8. The munition of claim 1, wherein said warhead and fuze are
standardized components having a standardized fuze well length and
fuze length, which define a length at the closed end of the fuze
well for a booster to detonate the warhead explosive, said booster
having less booster explosive such that said booster and said lens
fit in the defined length and produce a concentrated pressure wave
in the lobe having a peak pressure at least equal to that of the
larger booster.
9. (canceled)
10. (canceled)
11. The munition of claim 1, wherein said booster lens surface has
a parabolic shape around the booster explosive.
12. The munition of claim 11, wherein the booster further comprises
a housing for the booster explosive, said lens being formed into
said housing.
13. A fuze assembly for use in a fuze well of a warhead including a
warhead explosive around the fuze well, comprising: a booster
including a booster explosive; a fuze configured to detonate the
booster explosive to create a pressure wave having a forward axial
component and a radial component; and a booster lens having a
surface configured to re-direct a portion of the radial component
of the pressure wave off of the lens surface in the axial direction
to concentrate the pressure wave into a lobe with increased peak
pressure to penetrate the fuze well and directly detonate the
warhead approximately axially from the booster.
14. The fuze assembly of claim 13, wherein the peak pressure of the
booster pressure wave does not exceed a pressure threshold to
detonate the warhead explosive, said increased peak pressure of the
lobe exceeding the pressure threshold to directly detonate the
warhead explosive.
15. (canceled)
16. (canceled)
17. A booster for use with a fuze in a warhead, comprising: a
housing; an explosive pellet placed inside the housing; and a lens
formed into the walls of the housing having a surface configured to
re-direct and--concentrate a portion of a radial component of a
pressure wave caused by the detonation of the explosive pellet off
of the lens surface in the axial direction into a lobe in a
predetermined direction with increased pressure to penetrate and
directly detonate the warhead approximately axially from the
booster.
18. (canceled)
19. (canceled)
20. (canceled)
21. The booster of claim 17, wherein said lens surface has a
parabolic shape around the booster.
22-26. (canceled)
Description
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] This application claims benefit of priority under 35 U.S.C.
119(e) to U.S. Provisional Application No. 60/823,874 entitled
"Warhead Booster Explosive Lens" filed on Aug. 29, 2006, the entire
contents of which are incorporated by reference.
BACKGROUND OF THE INVENTION
[0002] 1. Field of the Invention
[0003] This invention relates to the explosive transfer between a
booster and a warhead.
[0004] 2. Description of the Related Art
[0005] The detonation of a warhead in a munition e.g., a missile,
projectile, artillery shell, bomb, etc. is typically a multi-stage
process to ensure both reliability and safety. It is important that
the warhead detonate when triggered and not detonate accidentally
due, for example, to mishandling or exposure to fire. The
consequences of accidental detonation at a munitions depot or
on-board a ship could be devastating. The explosive transfer
between the booster and warhead can be a very challenging problem
when trying to satisfy cost, interoperability, reliability and
safety concerns.
[0006] As shown in FIGS. 1a and 1b, an exemplary munition 10
includes a warhead 12, a fuze 14 and a booster 16. Warhead 12
includes an external housing 18, a fuze well 20 formed from steel
and lined with asphalt to provide insulation and protection from
expansion/contraction, a charge tube fitting 22 for routing
electrical cabling through the warhead to the fuze and explosive
material 24 filling the warhead. In this particular embodiment, the
fuze is not connected to electrical cabling through fitting 22 but
the general purpose warhead includes the fitting nonetheless.
Booster 16 includes an explosive pellet 26 that sits inside a
housing 32. The booster is placed on top of the fuze, directly on
top of the fuze's explosive pellet 34, and the assembly is inserted
into the warhead's fuze well. A locking mechanism 36 secures the
assembly.
[0007] To detonate the warhead, fuze 14 detonates its small
explosive pellet 34, which transfers a pressure wave to the booster
causing the booster explosive pellet 26 to detonate. Detonation of
the booster generates a much larger pressure wave that is
transferred to the warhead causing the warhead explosive 24 to
detonate. In order to detonate the warhead explosive, the booster
pressure wave that is transferred to the explosive material must
exceed a characteristic `detonation threshold` of the material. To
address safety concerns, modern insensitive munitions (IM)
compliant explosives are switching to explosive materials in the
warhead that have a higher detonation threshold. The other factor
that affects detonation transfer is the `barrier` between the
booster detonation and the warhead's explosive material. This
barrier includes the steel fuze well and asphalt lining and the
charge tube fitting that attenuate the pressure wave. The barrier
also includes any airgap between the fuze well and explosive
materials that will occur at low temperatures, which also
attenuates the pressure wave. To ensure reliability, explosive
transfer must be designed for the worst case conditions including
thickness of the barriers and extreme cold.
[0008] FIGS. 2 and 3 depict a simulation of explosive transfer in
which the warhead explosive failed to detonate because the booster
pressure wave 40 (dynes/cm.sup.2) that was transferred to the
explosive material 24 did not exceed the detonation threshold 42.
In the depicted warhead design, the detonation threshold occurs at
approximately 4.55.times.10.sup.10 dynes/cm.sup.2. As shown, the
pressure wave emanates fairly uniformly from the booster explosive
pellet 26 outward through the fuze well and into the warhead
explosive material except that the wave is heavily attenuated at
90.degree. from the booster interface by the charge tube fitting
22. Standard techniques to improve explosive transfer reliability
include increasing the explosive energy of the booster. However, in
the depicted simulation a 50% increase in explosive energy was
still not sufficient to detonate the warhead. Furthermore,
increasing the booster explosive increases costs, increases the
total amount of explosive in a depot or on-board ship and may not
tit in the available space in the fuze well in general purpose
warheads with standard fuzes. For both economic and reliability
reasons, the military places considerable demands on using proven
general purpose warhead designs and fuze interchanngeably in many
different weapons systems. Another known technique that was tried
was to include a `flyer plate` on top of the booster. Upon booster
detonation, the flyer plate is blasted forward so that its momentum
into the explosive material triggers detonation. Unfortunately the
charge tube fittings in a general purpose warhead lie directly in
the path of the flyer plate rendering it ineffective.
[0009] By raising the detonation threshold to address accidental
detonation, modern IM compliant explosives have made the task of
reliable explosive transfer between the booster and warhead more
difficult. A cost-effective solution for improving explosive
transfer that can be used with general purpose warheads and fuzes
is needed.
SUMMARY OF THE INVENTION
[0010] The present invention provides a cost-effective solution to
improve explosive transfer between booster and warhead that is
compatible with the existing base of general purpose warheads and
flexible to work with new warhead configurations.
[0011] This is accomplished by placing a booster lens in the fuze
well that concentrates the pressure wave to penetrate the fuze well
with a peak pressure that exceeds the detonation threshold and
detonate the warhead explosive. The booster lens can be configured
to control the direction of the concentrated lobe to penetrate the
fuze well where the barriers are low. In an embodiment for a
general purpose warhead, a radial lens re-directs a portion of the
axial component of the booster detonation in the radial direction
away from the charge tube fittings to penetrate and detonate the
warhead explosive approximately radially from the lens. The radial
lens is suitably positioned between the booster and the closed end
of the fuze well and has an annular surface that forms an angle
with the booster to re-direct the explosive force radially. In
another embodiment, an axial lens re-directs a portion of the
radial component of the booster detonation in the axial direction
to penetrate and detonate the warhead explosive approximately
axially from the lens. The axial lens is suitably positioned around
the booster in the fuze well and has a parabolic shape. The
booster-lens assembly may be designed to occupy no more space than
a standard booster and yet produce higher peak pressure and a more
reliable explosive transfer. As such, the booster-lens assembly is
ideally suited for use with general purpose warheads and existing
fuzes.
[0012] These and other features and advantages of the invention
will be apparent to those skilled in the art from the following
detailed description of preferred embodiments, taken together with
the accompanying drawings, in which:
BRIEF DESCRIPTION OF THE DRAWINGS
[0013] FIGS. 1a and 1b, as described above, are an exploded and
section view of a warhead, booster and fuze assembly;
[0014] FIG. 2, as described above, is a diagram of the pressure
wave of a simulated booster explosion that fails to detonate the
warhead explosive;
[0015] FIG. 3, as described above, is a plot of the pressure wave
against the angle from the lens-booster interface.
[0016] FIGS. 4a and 4b are an exploded and section view of a
warhead, booster and fuze assembly including a booster lens for
concentrating the pressure wave to detonate the warhead
explosive;
[0017] FIGS. 5a and 5b are diagrams of a standard booster of the
prior art and an integrated booster-lens assembly of the present
invention;
[0018] FIG. 6 is a diagram of the lens illustrating how the
pressure wave is concentrated in the radial direction;
[0019] FIGS. 7a and 7b are time-elapsed diagrams of the pressure
wave of a simulated booster explosion using the lens that achieves
detonation transfer;
[0020] FIG. 8 is a plot of the pressure wave against the angle from
the lens-booster interface for the parabolic lens for the radial
lens;
[0021] FIG. 9 is a plot of booster lens angle sensitivity;
[0022] FIG. 10 is a section view of an alternate warhead design in
which a parabolic lens is formed into the booster housing to
concentrate the shock wave in the axial direction; and
[0023] FIG. 11 is a plot of the pressure wave against the angle
from the lens-booster interface for the parabolic lens.
DETAILED DESCRIPTION OF THE INVENTION
[0024] The present invention provides a cost-effective solution to
improve explosive transfer between booster and warhead that is
compatible with the existing base of general purpose warheads and
flexible to work with new warhead configurations. A booster lens is
placed in the fuze well that concentrates the pressure wave to
penetrate the fuze well with a peak pressure that exceeds the
detonation threshold and detonate the warhead explosive. The
booster lens can be configured to control the direction of the
concentrated lobe to penetrate the fuze well where the barriers are
low.
[0025] To illustrate the ease with which the booster lens can be
implemented with a general purpose warhead and standard fuze and
the effectiveness of the lens, the invention will be described with
reference to the munition 10 illustrated in FIGS. 1a-1b. Like
numbers will be used to describe like components. This particular
embodiment is directed at a radial booster lens that re-directs a
portion of the axial component of the booster explosion in the
radial direction.
[0026] As shown in FIGS. 4a and 4b, booster 16 from the traditional
fuze-booster assembly has been replaced with a booster 50 and
booster lens 52. Booster 50 still suitably includes an explosive
pellet 54 that sits inside a housing 60. In some configurations,
for example when the booster is procurred or manufactured separate
from the fuze, the pellet is placed inside a cup with a cover to
avoid handling bare explosive, which in turn is placed inside the
housing. To accommodate the addition of the booster lens, the size
of the booster 50 and particularly the thickness of explosive
pellet 54 are reduced. If the same explosive material is used, the
total explosive energy released by the detonation of the booster
will be less than for booster 16. However, the placement of booster
lens 52 between the booster and the closed end of fuze well 20
sufficiently concentrates the energy, albeit lower in total, so
that the peak pressure of the concentrated lobe is actually higher
and sufficiently high to exceed the detonation threshold and
detonate the warhead explosive 24.
[0027] The booster and lens can be discrete components as shown
above or they can be integrated into a booster-lens assembly 70 as
shown in FIG. 5b. In this case, a housing 74 is made large enough
to accommodate the explosive pellet 54 with the lens shape formed
directly in the housing 74. In this embodiment, the booster-lens
assembly is formed with an axial conduit 82 for routing the
electrical cabling from the charge tube fittings to the fuze. In a
standard booster 83 as shown in FIG. 5a, the explosive pellet 84
fits inside a housing 86. If the booster-lens assembly 70 is
designed to replace a standard booster, the size of the housings
may be the same. Although the standard booster will have a larger
explosive pellet, hence greater total explosive energy, the
combination of the lens with a smaller pellet concentrates the
energy and thus provides a more reliable explosive transfer.
[0028] As shown in FIG. 6, in one embodiment booster lens 52 has a
base surface 90 that suitably rests on top of the booster and an
annular surface 92 that forms an acute non-zero angle with the top
of the booster. The sides and top surfaces of the lens suitably
conform to the closed-end of the fuze well. Detonation of the
booster's explosive pellet 54 generates a pressure wave 94 that has
a radial component 96 and an axial component 98. A portion of axial
component 98 is re-directed in the radial direction thereby
concentrating more energy in a lobe 100 that travels approximately
radially outward to penetrate the fuze well and detonate the
warhead explosive. The lens is suitably formed from a material such
as steel or aluminum that can absorb the booster detonation and
re-direct the energy without being instantly destroyed. The width
of base surface 90 and angle a of the annular surface 92 effect how
much of the axial component is captured, how tightly the energy is
concentrated in lobe 100 and in what direction lobe 100 is
oriented. The angle and base width are suitably selected to capture
a sizeable portion of the axial component and re-direct it into a
concentrated lobe so that the peak pressure is sufficiently high
for reliable explosive transfer. These parameters are constrained
by both the available diameter and thickness of the lens in a
particular booster-lens assembly and warhead design.
[0029] FIGS. 7a-7b and 8 depict a simulation of explosive transfer
using a booster-lens assembly in which the warhead explosive
successfully detonated 101 because the peak pressure in lobe 100 of
pressure wave 94 that was transferred to the explosive material
exceeded the detonation threshold 102, approximately
4.55.times.10.sup.10 dynes/cm.sup.2 for this design. As shown, the
pressure wave emanates in a narrow field of view from the booster
explosive pellet outward through the fuze well and into the warhead
explosive material. The wave is heavily concentrated in lobe 100
with a maximum pressure of approximately 2.75.times.10.sup.11
dynes/cm.sup.2 about 10-30.degree. above the radial direction and
is heavily attenuated with a minimum pressure of approximately
1.35.times.10.sup.9 dynes/cm.sup.2 elsewhere demonstrating that the
lens effectively redirected the energy towards the radial
direction. Although the total explosive energy may be a fraction,
e.g. 50%, of the standard booster for the described general purpose
warhead and fuze configuration, the peak pressure transferred to
the explosive material is significantly higher and thus much more
effective at producing a successful explosive transfer.
[0030] The simulation was ran for a range of lens angles and the
time to detonation was plotted 106, 108 for both a steel lens and
an aluminum lens as shown in FIG. 9. In both cases, explosive
transfer was achieved in a few tens of microseconds over a range of
at least 15-25 degrees. It can be extrapolated from these results
that a very fast and successful detonation corresponds to a highly
concentrated lobe with a high peak pressure. It is expected that
successful detonation would be achieved for angles well outside
this range. This particular simulation demonstrated that a
20.degree. angle was a good choice for the general purpose warhead
and standard fuze. The data suggests that an angle between
approximately 10.degree. and 30.degree. would provide reliable
explosive transfer for a general purpose warhead. Angles outside
this range and different ranges of angles will be dictated by the
design of the warhead, fuze and types and amounts of explosives
used.
[0031] Although the booster-lens assembly of the current invention
is particularly well-suited for use with the general purpose
warhead and interchangeable fuze, it is not so limited. The
principle of using the lens to concentrate and redirect the
pressure to penetrate a portion of the fuze well having a low
barrier can be extended to other existing or new warhead designs.
The lens can be used to increase the reliability of explosive
transfer for a given booster or can be used to provide reliable
explosive transfer for a smaller booster. The booster-lens assembly
can be configured to fit into a predefined space in the fuze well
or configured for use in a new design that is not so
constrained.
[0032] As illustrated in FIGS. 10 and 11, an axial booster lens 120
re-directs a portion of the radial component 122 of the booster
detonation in the axial direction to produce a concentrated axial
lobe 124 that penetrates and detonates the warhead explosive
approximately axially from the lens. The axial lens is suitably
positioned at the end of fuze 126 around the booster explosive 128
in the fuze well 130 and preferably has a parabolic shape. The
axial lens 120 is suitably formed into the walls of a housing 131
around the booster. The parabolic focus 132 at the initiation point
is positioned at the bottom of lens 120 at the interface with the
booster explosive 128. This configuration may be useful, for
example, in a warhead that does not have the charge tube fittings
positioned along the long axis of the warhead.
[0033] While several illustrative embodiments of the invention have
been shown and described, numerous variations and alternate
embodiments will occur to those skilled in the art. Such variations
and alternate embodiments are contemplated, and can be made without
departing from the spirit and scope of the invention as defined in
the appended claims.
* * * * *