US3896731A - Explosive initiator device - Google Patents
Explosive initiator device Download PDFInfo
- Publication number
- US3896731A US3896731A US083260A US8326070A US3896731A US 3896731 A US3896731 A US 3896731A US 083260 A US083260 A US 083260A US 8326070 A US8326070 A US 8326070A US 3896731 A US3896731 A US 3896731A
- Authority
- US
- United States
- Prior art keywords
- explosive
- plate
- charges
- lowermost
- plate members
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C19/00—Details of fuzes
- F42C19/08—Primers; Detonators
- F42C19/0838—Primers or igniters for the initiation or the explosive charge in a warhead
- F42C19/0846—Arrangements of a multiplicity of primers or detonators, dispersed within a warhead, for increased efficiency
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42D—BLASTING
- F42D1/00—Blasting methods or apparatus, e.g. loading or tamping
- F42D1/04—Arrangements for ignition
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S102/00—Ammunition and explosives
- Y10S102/701—Charge wave forming
Definitions
- the device comprises four circular plates arranged in a stacked configuration with each plate including an arrangement of intersecting slots 24 2 M. 0 -6 I 2'. D 2D /2 24 2 OFOO ll l am 2/ 9 21 c 2 4 F [52] U.S. [51] Int. Cl. [58] Field of Search point of intersection of an arrangement of slots in a subjacent plate.
- the up- [56] References Cited UNITED STATES PATENTS permost plate has four explosive terminations, the plate subjacent thereto sixteen, the next subjacent 102/22 plate fifty-two with the lowermost plate having fifty- 102/22 two explosive charges. 4/1969 Stresau 102/22 3,016,831 l/l962 Coursenestablished briefly 3,311,055 3/1967 Stresau, Jr. et al.. 3,430,563
- This invention relates generally to explosive initiators and more particularly to a multipoint simultaneous explosive initiating device.
- an explosive charge in which the generated detonation front arrives simultaneously at a plurality of predetermined points on a particular geometric surface. It has been found practical, for example, to emboss a metal surface by means of a detonation front which is made to arrive simultaneously at a plurality of points on the surface of the metal. Further, by placing the surface at which the plurality of simultaneous explosive initiations occur in abutting relationship with the surface of a block of homogeneous explosive material a plane explosive detonation wavemay be generated within the block of explosive.
- the use of such a device is important in basic scientific investigations of explosive phenomena such, for example, as the exceedingly high pressures of short duration created upon the simultaneous ignition of a plurality of points on a particular surface. Recently, a need has arisen in applications such as those mentioned hereinbefore, for such a simultaneous detonation system to be operable in high temperature environments.
- detonation systems have been devised in various forms.
- One such system utilizes a large number of electric initiators.
- Another comprises apparatus in which the detonation wave is transmitted between charges by flying plates or fragments.
- systems utilizing stacked configurations such as multiple layers of flexible sheet explosive material separated and supported by an inert elastomer and systems having a plurality of layers of a tap-sensitive high explosive with each explosive layer being separated from the adjacent layer by a barrier plate provided with an array of detonation-transmitting channels have been used with some degree of success.
- none of the aforementioned devices have been designed to be used with heat resistant explosives which expression, for the instant purposes defines those explosives having a melting point above 300 C and a vacuum thermal stability such that they decompose at a rate less than 2.0 cc/gm/hr at 260 C.
- one object of this invention is to provide a new and improved explosive device in which a detonation that originates at a single point therein arrives simultaneously at a plurality of points on a surface.
- Another object of the invention is the provision of a new and improved detonation initiating and wave shaping device having substantial strength characteristics.
- Still another object of the present invention is to provide a new and improved explosive detonation device utilizable with heat resistant explosives.
- a further object of the instant invention is to provide a new and improved detonation wave shaping system which may utilize mild detonating cord to transmit a detonation front from a single detonation point in one plane simultaneously to a plurality of detonation points in another plane.
- these and other objects are attained by providing a stacked array of a plurality of plates wherein the path of detonation transfer from a centrally located position in the uppermost plate is converted into an increasing number of detonations effected by configurations of detonating cords of geometric symmetry and of equal lengths in each successive plate, finally terminating in a series of points of simultaneous explosive initiations in the lowermost plate.
- FIG. 1 is a plan view of the explosive detonation device of the present invention illustrating the various paths along which the detonation front travels;
- FIG. 2 is a cross-sectional view of the device taken along line 22 of FIG. 1;
- FIGS. 3(a) to 3(d) are perspective views of the individual plates which comprise the device
- FIG. 4 is a sectional view of a typical detonating cord and the apparatus associated therewith used to transmit the detonation wave through the device;
- FIG. 5 is a plan view of a typical assembly of detonating cords with a modification thereof shown in phantom;
- FIG. 6 is a side view of the assembly of FIG. 5;
- FIG. 7 is a partial cross-sectional view of the device taken along line 77 of FIG. 1;
- FIG. 8 is a sectional view of an explosive charge of the present invention.
- FIG. 9 is a sectional view of an explosive lead of the present invention.
- the explosive initiator of the present invention is shown as including a series of thin circular plates 10, 12, 14 and 16 which are stacked superjacently in a concentric and contacting fashion.
- the plates are preferably made of a suitable inert metallic material, such for example, as aluminum. They also may be made of wood if dimensional tolerances can be achieved.
- the uppermost plate 16 has the smallest diameter of the plates with plate 14 being next in size. Plates and 12 are of equal diameter with plate 10 being the lowermost plate.
- Plate 16 is shown as having four radial slots 18 formed therein emanating from the center of the plate at right angles to each other forming an effective intersection point 20.
- Each of slots 18 is so formed as to be receivable of a length of heat resistant mild detonating cord 22, as best seen in FIG. 2, and which will be described in greater detail hereinafter.
- the terminal end 24 of each slot 18 extends through the plate 16 as best shown in FIG. 2.
- Plate 14 as shown in FIG. 3(b), has four arrangements of slots 26 formed therein with each arrangement in the shape ofa cross having four arms intersecting at 30 with the ends of three of these arms bent at right angles.
- the fourth leg of each arrangement is elongated, as at 28, for purposes which will be made more apparent hereinafter.
- the slots 26 in plate 14, similarly to the slots 18 of plate 16 are adapted to receive mild detonating cord described hereinafter.
- the terminal points 24 of the slots 26 extend through the plate 14.
- plates 16 and 14 are such that when plate 16 is placed in position over plate 14 the terminal ends 24 of the slots in plate 16 are positioned directly above the four intersection points 30 of slots 26 in plate 14. This strategic positioning of the plates is essential to the proper functioning of the device as will be more fully explained hereinafter.
- plate 12 has twelve crossshaped slot configurations 32 each having points of intersection formed therein.
- the slots 32 are substantially identical to the slots of plate 16 except reduced in length.
- intersection points 34 of each slot arrangement 32 in plate 12 are directly subjacent to the terminal points 24 of the slots 26 of plate 14.
- plate 10 comprises a plurality of equally spaced cylindrical cavities 36 which extend through the plate 10 and which houses individual explosive charges 38.
- the spacing of the cavities 36 is determined by the positions of the terminal points 24 of slots 32 in plate 12, that is, the cavities 36 are positioned such that when plate 10 is in position beneath plate 12 each of cavities 36 lies directly beneath a terminal end 24 in plate 12.
- a typical length of heat resistant mild detonating cord 22 is illustrated in FIG. 4 as having one end connected to a cup-shaped cap 40 containing a heat resistant explosive 42 and its other end connected to a base charge 44 of a heat resistant explosive by an end coupler 46.
- This cord structure is described in applicants copending application Ser. No. 475,035, filed July 26, 1965. It includes a mild detonating cord which comprises a cylindrical metallic sheath 48, preferably made of a lead alloy, having an inner diameter of approximately 0.025 inches and is filled with a heat resistant explosive 50.
- heat resistant explosives are DIPAM (dipicramid), HNS (hexanitrostilbene), NONA (nonanitroterphenyl), and the like.
- a heat resistant mild detonating cord has a lower intensity detonation front than a conventional mild detonating cord, when the'detonation front from a small diameter heat resistant mild detonating cord travels into a substantially larger diameter base charge of a heat resistant explosive degradation of that wave front occurs and the base charge does not detonate.
- the end coupler 46 includes an elongate metallic housing 52 having a frusto conical recess 54 axially formed in one portion thereof and a communicating axial cylindrical bore 56 formedin the other portion thereof, defining an annular shoulder 58 therebetween.
- the end coupler 46 provides for amplification of the detonation front generated by ignition of the heat resistant mild detonating cord 18 to a magnitude sufficient to initiate the base charge 44.,Cord 22 is inserted into the axial bore 56until the end thereof abuts the annular shoulder 58.
- a suitable adhesive (not shown), such as epoxy resin or other potting composition, may be employed to bond the end of the cord within the end coupler 46
- the frusto-conical recess 54 is filled with a booster charge 60 of I-INS (Grade 1) explosive.
- I-INS .(Grade 1) isa superfine grade of hexanitrostilbene prepared by the method disclosed in US. Pat. No. 3,505,4l3 issued on Apr. 7, 1970 to Kathryn G. Shipp. It has been found that if it is attempted to utilize other explosives for the booster charge rather than the I-INS (Grade 1) type boostercharge, the shock wave deteriorates rather than amplifies and hence does not detonate the base charge 24.
- the explosives contained in the end coupler 46 are held therein by a cylindrical cap. member 62 opened at one end thereof which is crimped over metallic housing 52 so, as to be fixed in place.
- FIGS. 5 and 6 an assembly 64 of four lengths of mild detonating cord 22 is shown as composed of four individual lengths of cord arranged as the arms of a cross .with their abutting ends connected to explosive-filled caps 40.
- a ring-shaped manifold 66 is provided having suitable apertures 68 to accommodate the caps 40 and thereby retains the assembly 64 in the desired-configuration.
- Thecords may be shaped in any desired manner, such, for example, as by turning the opposite ends having end coupler 46 downward as at 70 as depicted in FIG. 6...
- the cord assembly 64 is disposed in the slots 18 in top plate 16.
- the slots are turned in a downward direction at the ends 24 thereof to accommodate the end couplers 46 at the ends of each cord 22.
- the slot ends 24 communicate with the underside of plate- 16 forming a through-bore to allow the tip of the end couplers to be'flush with the lower face of plate 16. It is-to be noted that the intersection point 20 iswidened in the central portion of the plate 16 to accommodate-the ring manifold 66.
- the ability of the mild detonating cord to be bent in right angles as, for example, at 72 (FIG. 5) enables the mild detonating cord assemblies to be suitably placed within the slots 26 in plate 14.
- the general configuration of the detonating cord assembly is similar to the configuration employed for plate 16, i.e., the cap 40 at the ends of the individual cords are held in abutting relationship by a ring-shaped manifold 66 with the cords extending outwardly at right angles to the two immediate adjacent cords. As shown by phantom lines, three of the cords are merely twisted in a right angle bend while the fourth cord is suitably extended to form the appropriate configuration for.plate- 14. As hereinbefore stated,
- the terminal points 24 of the slots.26 communicate with 'the lower surface of plate;l4 thereby permitting the mend surfacelof end, coupler 46 to be flush with the lower surface as best seen in FIG. 2.
- explosive charge 38 is composed of a substantially cube-shaped metallic cup 80 having an opening 82 on one end thereof and being filled with" an RDX (cyclotrimethylenetrinitramine) composition explosive 84 containing approximately 98% RDX and 2% calcium stearate pressed at 10,000 psi.
- the opening 82 is closed by a thin metallic closure disc 86.
- the explosive lead 78 is substan-'* tially cylindrical and preferably includes three equal increments of l-INS explosive 88 compressed at approximately 16,000 psi.
- the explosive is contained in an aluminum cylindrical cup 90 having an opening 92 at one end thereof wherein an aluminum closure disc 94' is positioned serving to close opening 92.
- the slots in plates 12, 14 and 16 are first filled with a suitable adhesive, such for example, as General Electric RTV 1 12 silicone rubber adhesive and the mild detonating cord assemblies subsequently positioned therein.
- a suitable adhesive such for example, as General Electric RTV 1 12 silicone rubber adhesive and the mild detonating cord assemblies subsequently positioned therein.
- the plates are fastened together by conventional means, such as bolts 96 (FIG. 1), which also serve to align the plates in the desired relative orientations with respect to each other.
- An explosive initiating device comprising:
- each of said detonating cords having a first explosive charge and a base charge connected to opposite ends thereof,
- each of said first explosive charges being disposed at a juncture of each said arrangements formed by said commonly joined detonating cords and each of said base charges being disposed in a through bore formed in all but said lowermost one of said plate members,
- said housing having a frusto-conical recess formed in one end thereof; said housing having an axial bore formed in the other end thereof and intersecting said frusto-conical recess; and said frusto-conical recess being filled with hexanitrostilbene (Grade 1) explosive.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Abstract
A device for simultaneously transferring a single explosive detonation from an initial detonation point to a plurality of detonation points. The device comprises four circular plates arranged in a stacked configuration with each plate including an arrangement of intersecting slots in which lengths of heat resistant mild detonating cord are positioned terminating in explosive booster ends. The explosive booster end of each detonating cord is positioned superjacently to the point of intersection of an arrangement of slots in a subjacent plate. In a preferred embodiment, the uppermost plate has four explosive terminations, the plate subjacent thereto sixteen, the next subjacent plate fifty-two with the lowermost plate having fiftytwo explosive charges.
Description
[ July 29, 1975 Unite States atent [1 1 Kilmer EXPLOSIVE INITIATOR DEVICE Primary ExaminerVerlin R. Pendegrass [75] Inventor: Earl Kumer College Park, Md Attorney, Agent, or FirmR. S. Sciascia; J. A. Cooke ABSTRACT A device for simultaneously transferring a single ex- [73] Assignee: The United States of America as represented by the Secretary of the Navy, Washington, DC.
Sept. 22, 1970 Appl. No.: 83,260
[22] Filed plosive detonation from an initial detonation point to a plurality of detonation points. The device comprises four circular plates arranged in a stacked configuration with each plate including an arrangement of intersecting slots 24 2 M. 0 -6 I 2'. D 2D /2 24 2 OFOO ll l am 2/ 9 21 c 2 4 F [52] U.S. [51] Int. Cl. [58] Field of Search point of intersection of an arrangement of slots in a subjacent plate. In a preferred embodiment, the up- [56] References Cited UNITED STATES PATENTS permost plate has four explosive terminations, the plate subjacent thereto sixteen, the next subjacent 102/22 plate fifty-two with the lowermost plate having fifty- 102/22 two explosive charges. 4/1969 Stresau 102/22 3,016,831 l/l962 Coursen................................ 3,311,055 3/1967 Stresau, Jr. et al.. 3,430,563
3 Claims, 12 Drawing Figures FATENTEB JUL29 1975 Ear! E: Kilmer INVENTOR ATTRNFY PATENTED JUL 2 91975 SHEET QOOOOOO FE. 3w;
EXPLOSIVE INITIATOR DEVICE BACKGROUND OF THE INVENTION This invention relates generally to explosive initiators and more particularly to a multipoint simultaneous explosive initiating device.
In many diverse applications it is desirable to employ an explosive charge in which the generated detonation front arrives simultaneously at a plurality of predetermined points on a particular geometric surface. It has been found practical, for example, to emboss a metal surface by means of a detonation front which is made to arrive simultaneously at a plurality of points on the surface of the metal. Further, by placing the surface at which the plurality of simultaneous explosive initiations occur in abutting relationship with the surface of a block of homogeneous explosive material a plane explosive detonation wavemay be generated within the block of explosive. The use of such a device is important in basic scientific investigations of explosive phenomena such, for example, as the exceedingly high pressures of short duration created upon the simultaneous ignition of a plurality of points on a particular surface. Recently, a need has arisen in applications such as those mentioned hereinbefore, for such a simultaneous detonation system to be operable in high temperature environments.
In the past, detonation systems have been devised in various forms. One such system utilizes a large number of electric initiators. Another comprises apparatus in which the detonation wave is transmitted between charges by flying plates or fragments. In addition, systems utilizing stacked configurations such as multiple layers of flexible sheet explosive material separated and supported by an inert elastomer and systems having a plurality of layers of a tap-sensitive high explosive with each explosive layer being separated from the adjacent layer by a barrier plate provided with an array of detonation-transmitting channels have been used with some degree of success.
However, almost all of these prior art systems possess certain distinct disadvantages. Inherent in each of them is the use of highly sensitive explosive materials. As a consequence, it is not uncommon to have a premature initiation of a few of the points on the surface due to the extreme sensitivity of the explosive employed. The multiple electric detonator systems involve both costly and bulky apparatus while the moving metal detonator systems must be especially designed for each detonation wave configuration desired. Moreover, none of these systems give any degree of structural integrity when used in circumstances requiring a high degree of strength and rigidity such, for example, as when the initiator is desired to physically separate two compartments in a vehicle, such as a torpedo. Finally, none of the aforementioned devices have been designed to be used with heat resistant explosives which expression, for the instant purposes defines those explosives having a melting point above 300 C and a vacuum thermal stability such that they decompose at a rate less than 2.0 cc/gm/hr at 260 C.
The primary reason for the inability of the prior art devices to use heat resistant explosives is that the shock intensity of the detonation front developed by the heat resistant explosive is substantially smaller than the shock intensity of the detonation front developed by conventional explosives. For this reason it has been impractical until recently to employ a heat resistant explosive in a multipoint simultaneous detonation system.
Accordingly, one object of this invention is to provide a new and improved explosive device in which a detonation that originates at a single point therein arrives simultaneously at a plurality of points on a surface.
Another object of the invention is the provision of a new and improved detonation initiating and wave shaping device having substantial strength characteristics.
Still another object of the present invention is to provide a new and improved explosive detonation device utilizable with heat resistant explosives.
A further object of the instant invention is to provide a new and improved detonation wave shaping system which may utilize mild detonating cord to transmit a detonation front from a single detonation point in one plane simultaneously to a plurality of detonation points in another plane.
Briefly, in accordance with one embodiment of this invention, these and other objects are attained by providing a stacked array of a plurality of plates wherein the path of detonation transfer from a centrally located position in the uppermost plate is converted into an increasing number of detonations effected by configurations of detonating cords of geometric symmetry and of equal lengths in each successive plate, finally terminating in a series of points of simultaneous explosive initiations in the lowermost plate.
BRIEF DESCRIPTION OF THE DRAWING A more complete appreciation of the invention and many of the attendant advantages thereof will be readily appreciated as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein:
FIG. 1 is a plan view of the explosive detonation device of the present invention illustrating the various paths along which the detonation front travels;
FIG. 2 is a cross-sectional view of the device taken along line 22 of FIG. 1;
FIGS. 3(a) to 3(d) are perspective views of the individual plates which comprise the device;
FIG. 4 is a sectional view of a typical detonating cord and the apparatus associated therewith used to transmit the detonation wave through the device;
FIG. 5 is a plan view of a typical assembly of detonating cords with a modification thereof shown in phantom;
FIG. 6 is a side view of the assembly of FIG. 5;
FIG. 7 is a partial cross-sectional view of the device taken along line 77 of FIG. 1;
FIG. 8 is a sectional view of an explosive charge of the present invention; and
FIG. 9 is a sectional view of an explosive lead of the present invention.
DESCRIPTION OF THE PREFERRED EMBODIMENT Referring now to the drawings wherein like reference characters designate identical or corresponding parts throughout the several views, and more particularly to FIGS. 1 and 2 thereof, the explosive initiator of the present invention is shown as including a series of thin circular plates 10, 12, 14 and 16 which are stacked superjacently in a concentric and contacting fashion.
The plates are preferably made of a suitable inert metallic material, such for example, as aluminum. They also may be made of wood if dimensional tolerances can be achieved. The uppermost plate 16 has the smallest diameter of the plates with plate 14 being next in size. Plates and 12 are of equal diameter with plate 10 being the lowermost plate.
Referring now to FIG. 3(a). Plate 16 is shown as having four radial slots 18 formed therein emanating from the center of the plate at right angles to each other forming an effective intersection point 20. Each of slots 18 is so formed as to be receivable of a length of heat resistant mild detonating cord 22, as best seen in FIG. 2, and which will be described in greater detail hereinafter. The terminal end 24 of each slot 18 extends through the plate 16 as best shown in FIG. 2.
Referring back to FIG. 1, it will be noted that the geometry of plates 16 and 14 is such that when plate 16 is placed in position over plate 14 the terminal ends 24 of the slots in plate 16 are positioned directly above the four intersection points 30 of slots 26 in plate 14. This strategic positioning of the plates is essential to the proper functioning of the device as will be more fully explained hereinafter.
As shown in FIG. 3(a), plate 12 has twelve crossshaped slot configurations 32 each having points of intersection formed therein. The slots 32 are substantially identical to the slots of plate 16 except reduced in length. When placed in position beneath plate 14 the intersection points 34 of each slot arrangement 32 in plate 12 are directly subjacent to the terminal points 24 of the slots 26 of plate 14.
As shown in FIG. 3(d), plate 10 comprises a plurality of equally spaced cylindrical cavities 36 which extend through the plate 10 and which houses individual explosive charges 38. The spacing of the cavities 36 is determined by the positions of the terminal points 24 of slots 32 in plate 12, that is, the cavities 36 are positioned such that when plate 10 is in position beneath plate 12 each of cavities 36 lies directly beneath a terminal end 24 in plate 12.
A typical length of heat resistant mild detonating cord 22 is illustrated in FIG. 4 as having one end connected to a cup-shaped cap 40 containing a heat resistant explosive 42 and its other end connected to a base charge 44 of a heat resistant explosive by an end coupler 46. This cord structure is described in applicants copending application Ser. No. 475,035, filed July 26, 1965. It includes a mild detonating cord which comprises a cylindrical metallic sheath 48, preferably made of a lead alloy, having an inner diameter of approximately 0.025 inches and is filled with a heat resistant explosive 50. Examples of heat resistant explosives are DIPAM (dipicramid), HNS (hexanitrostilbene), NONA (nonanitroterphenyl), and the like.
Since a heat resistant mild detonating cord has a lower intensity detonation front than a conventional mild detonating cord, when the'detonation front from a small diameter heat resistant mild detonating cord travels into a substantially larger diameter base charge of a heat resistant explosive degradation of that wave front occurs and the base charge does not detonate.
The end coupler 46 includes an elongate metallic housing 52 having a frusto conical recess 54 axially formed in one portion thereof and a communicating axial cylindrical bore 56 formedin the other portion thereof, defining an annular shoulder 58 therebetween. The end coupler 46 provides for amplification of the detonation front generated by ignition of the heat resistant mild detonating cord 18 to a magnitude sufficient to initiate the base charge 44.,Cord 22 is inserted into the axial bore 56until the end thereof abuts the annular shoulder 58. A suitable adhesive (not shown), such as epoxy resin or other potting composition, may be employed to bond the end of the cord within the end coupler 46 The frusto-conical recess 54 is filled with a booster charge 60 of I-INS (Grade 1) explosive. I-INS .(Grade 1) isa superfine grade of hexanitrostilbene prepared by the method disclosed in US. Pat. No. 3,505,4l3 issued on Apr. 7, 1970 to Kathryn G. Shipp. It has been found that if it is attempted to utilize other explosives for the booster charge rather than the I-INS (Grade 1) type boostercharge, the shock wave deteriorates rather than amplifies and hence does not detonate the base charge 24. The explosives contained in the end coupler 46 are held therein by a cylindrical cap. member 62 opened at one end thereof which is crimped over metallic housing 52 so, as to be fixed in place.
Turning now to FIGS. 5 and 6, an assembly 64 of four lengths of mild detonating cord 22 is shown as composed of four individual lengths of cord arranged as the arms of a cross .with their abutting ends connected to explosive-filled caps 40. A ring-shaped manifold 66 is provided having suitable apertures 68 to accommodate the caps 40 and thereby retains the assembly 64 in the desired-configuration. Thecords may be shaped in any desired manner, such, for example, as by turning the opposite ends having end coupler 46 downward as at 70 as depicted in FIG. 6...
As shown in FIG. 2, the cord assembly 64 is disposed in the slots 18 in top plate 16. As hereinbefore set forth, the slots are turned in a downward direction at the ends 24 thereof to accommodate the end couplers 46 at the ends of each cord 22.,The slot ends 24 communicate with the underside of plate- 16 forming a through-bore to allow the tip of the end couplers to be'flush with the lower face of plate 16. It is-to be noted that the intersection point 20 iswidened in the central portion of the plate 16 to accommodate-the ring manifold 66.
The ability of the mild detonating cord to be bent in right angles as, for example, at 72 (FIG. 5) enables the mild detonating cord assemblies to be suitably placed within the slots 26 in plate 14. The general configuration of the detonating cord assembly, as depicted in phantom lines in FIG. 5, is similar to the configuration employed for plate 16, i.e., the cap 40 at the ends of the individual cords are held in abutting relationship by a ring-shaped manifold 66 with the cords extending outwardly at right angles to the two immediate adjacent cords. As shown by phantom lines, three of the cords are merely twisted in a right angle bend while the fourth cord is suitably extended to form the appropriate configuration for.plate- 14. As hereinbefore stated,
the terminal points 24 of the slots.26 communicate with 'the lower surface of plate;l4 thereby permitting the mend surfacelof end, coupler 46 to be flush with the lower surface as best seen in FIG. 2.
It is to be noted that there are four charge cavities 74 in plate 10 as shown in ,Fl G." 3(d)which upon assembly of the device will'rio't lie beneath any termin'al'point 24 of slots 32 in plate 12. The four explosive charges 38 housed in these four cavities are necessary to maintain the uniform nature of the detonation wave created upon the simultaneous ignition of the explosive charges 38 as will be discussed hereinafter in the operation of the invention. In plate 12 directly above the four cavities 74 of plate 10, as shown in FIGS. 3(a) and 7, are four cylindrical explosive lead cavities 76 which house cylindrical explosive leads 78. Suprajacent the explosive lead cavities 76, positioned in plate 12, is an end coupler 46 which is connected to the end of a length of mild detonating cord 22 which itself comprises the elongated leg 28 of the detonating cord assemblies 64 of plate 14.
As shown in FIG. 8, explosive charge 38 is composed of a substantially cube-shaped metallic cup 80 having an opening 82 on one end thereof and being filled with" an RDX (cyclotrimethylenetrinitramine) composition explosive 84 containing approximately 98% RDX and 2% calcium stearate pressed at 10,000 psi. The opening 82 is closed by a thin metallic closure disc 86.
The explosive lead 78, as shown in FIG. 9, is substan-'* tially cylindrical and preferably includes three equal increments of l-INS explosive 88 compressed at approximately 16,000 psi. The explosive is contained in an aluminum cylindrical cup 90 having an opening 92 at one end thereof wherein an aluminum closure disc 94' is positioned serving to close opening 92.
In assembly, the slots in plates 12, 14 and 16 are first filled with a suitable adhesive, such for example, as General Electric RTV 1 12 silicone rubber adhesive and the mild detonating cord assemblies subsequently positioned therein. The plates are fastened together by conventional means, such as bolts 96 (FIG. 1), which also serve to align the plates in the desired relative orientations with respect to each other.
In the operation of the device a fundamental law is relied upon which makes possible the successful operation thereof; i.e., a homogeneous explosive mass normally detonates at uniform velocity in all directions. Therefore, an explosive initiation occurring at the effective intersection point of the explosive cord assembly will create separate detonation waves in each length of cord which will travel outward at equal velocities and reach the end couplers 46 at the same instant. It may thus be seen that all of the paths between the initial point of initiation at the intersection point 20 of slots in plate 16 and each explosive charge 38 in plate 10 must be of equal length. This requirement, therefore, determines the configuration of the elongate leg 28 of the cord arrangements 64 and slot arrangements 26 of plate 14, i.e., the length of the path from the slot intersection point 30 of plate 14 through the elongated leg 28 to and through the explosive lead 78 and terminating at an explosive charge 56 is equal to the length of the path from the point of the slot intersection 30 through a normal leg of slot arrangement 26 to the intersection point 34 of slots 32 in plate 12, through a leg of one cross-shaped slot arrangement 32, and termisimultaneous. l t I A A typical detonation transfer-from an end coupler 46,
for example, in plate 16 to a detonating cord in plate 14 occurs when the mild detonating cord is ignited, thereby creating a detonation front which travels through the cord and is amplified by end coupler 46 to a sufficient magnitude to effect the initiation of base charge 44 therein. Upon the initiation of base charge 44 the cup member 62 bursts and the expanding hot gases and fragments resulting therefrom penetrate the four caps 40 located directly therebeneath and initiate the explosive 42 contained therein thereby causing detonation fronts to be set up in the detonating cords in plate 14. A similar sequence is undergone in the case of an end coupler 46 at the end of an elongated leg 28 igniting an explosive lead 78 and also when the explosive charges 38 are ignited by the end couplers 46 or leads 78.
Obviously, numerous modifications and variations of the present invention are possible in light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described herein.
What is claimed as new and desired to be secured by Letters Patent of the United States is:
1. An explosive initiating device comprising:
a plurality of contacting, superjacently stacked plate members;
a plurality of arrangements of commonly joined mutually perpendicular mild detonating cords positioned within slots in said members, said arrangements disposed in progressively increasing numbers on all but the lowermost one of said superjacent plate members,
each of said detonating cords having a first explosive charge and a base charge connected to opposite ends thereof,
each of said first explosive charges being disposed at a juncture of each said arrangements formed by said commonly joined detonating cords and each of said base charges being disposed in a through bore formed in all but said lowermost one of said plate members,
each of said junctures of each of said detonating cord arrangements on all but the uppermost and lowermost ones of said plate members being located subjacent of the respective ones of said base charges of a superjacent one of said plate members; and
a plurality of second explosive charges disposed on equidistantly spaced through bores formed in said lowermost plate member, the majority of said through bores in said lowermost plate being positioned immediately subjacent of the base charges of a superjacent one of said plate members;
wherein the overall length of the respective paths from a point of initiation on the uppermost one of said plate members to each of said second explosive charges is equal, thereby affording a simultaneous initiation of said second explosive charges in said lowermost plate member in response to the inii 8 said housing having a frusto-conical recess formed in one end thereof; said housing having an axial bore formed in the other end thereof and intersecting said frusto-conical recess; and said frusto-conical recess being filled with hexanitrostilbene (Grade 1) explosive.
Claims (3)
1. An explosive initiating device comprising: a plurality of contacting, superjacently stacked plate members; a plurality of arrangements of commonly joined mutually perpendicular mild detonating cords positioned within slots in said members, said arrangements disposed in progressively increasing numbers on all but the lowermost one of said superjacent plate members, each of said detonating cords having a first explosive charge and a base charge connected to opposite ends thereof, each of said first explosive charges being disposed at a juncture of each said arrangements formed by said commonly joined detonating cords and each of said base charges being disposed in a through bore formed in all but said lowermost one of said plate members, each of said junctures of each of said detonating cord arrangements on all but the uppermost and lowermost ones of said plate members being located subjacent of the respective ones of said base charges of a superjacent one of said plate members; and a plurality of second explosive charges disposed on equidistantly spaced through bores formed in said lowermost plate member, the majority of said through bores in said lowermost plate being positioned immediately subjacent of the base charges of a superjacent one of said plate members; wherein the overall length of the respective paths from a point of initiation on the uppermost one of said plate members to each of said second explosive charges is equal, thereby affording a simultaneous initiation of said second explosive charges in said lowermost plate member in response to the initiation of the intersecting mild detonating cord of said uppermost plate member.
2. A device as recited in claim 1 wherein said base charge and said first and second explosive charges comprise heat resistant explosive materials.
3. A device as recited in claim 2 wherein said base charge is connected to the end of said detonating cord by an end coupler comprising: an elongated housing; said housing having a frusto-conical recess formed in one end thereof; said housing having an axial bore formed in the other end thereof and intersecting said frusto-conical recess; and said frusto-conical recess being filled with hexanitrostilbene (Grade 1) explosive.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US083260A US3896731A (en) | 1970-09-22 | 1970-09-22 | Explosive initiator device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US083260A US3896731A (en) | 1970-09-22 | 1970-09-22 | Explosive initiator device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3896731A true US3896731A (en) | 1975-07-29 |
Family
ID=22177194
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US083260A Expired - Lifetime US3896731A (en) | 1970-09-22 | 1970-09-22 | Explosive initiator device |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3896731A (en) |
Cited By (33)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4145972A (en) * | 1976-12-17 | 1979-03-27 | The United States Of America As Represented By The Secretary Of The Navy | Dual-mode warhead initiation system |
| EP0030189A1 (en) * | 1979-12-03 | 1981-06-10 | Aerospatiale Societe Nationale Industrielle | Multiway connector and process for transmitting pyrotechnical signals |
| US4282814A (en) * | 1974-12-20 | 1981-08-11 | The United States Of America As Represented By The Secretary Of The Navy | Dual-end warhead initiation system |
| US4475461A (en) * | 1981-06-17 | 1984-10-09 | The United States Of America As Represented By The Secretary Of The Navy | Monolithic multi-point warhead initiator |
| US4499828A (en) * | 1983-06-01 | 1985-02-19 | The United States Of America As Represented By The United States Department Of Energy | Barrier breaching device |
| DE3503013C1 (en) * | 1985-01-30 | 1986-06-26 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Safety device |
| FR2601126A1 (en) * | 1986-07-03 | 1988-01-08 | Matra Manurhin Defense | Primer pyrotechnic chain with shutter |
| US4784062A (en) * | 1986-07-31 | 1988-11-15 | Diehl Gmbh & Co. | Fuze for a projectile-forming charge |
| US4899663A (en) * | 1989-02-15 | 1990-02-13 | Automotive Systems Laboratory, Inc. | Percussion initiated inflator assembly |
| US6220166B1 (en) * | 1999-08-02 | 2001-04-24 | Sandia Corporation | Apparatus and method for producing fragment-free openings |
| RU2203260C2 (en) * | 1996-01-11 | 2003-04-27 | Дзе Энсайн-Бикфорд Компани | Detonators having inputs with many lines |
| RU2226254C2 (en) * | 2002-04-22 | 2004-03-27 | Российский Федеральный Ядерный Центр - Всероссийский Научно-Исследовательский Институт Экспериментальной Физики | Device for forming explosion wave |
| US6817297B1 (en) * | 2003-01-09 | 2004-11-16 | The United States Of America As Represented By The Secretary Of The Navy | Low-cost, no-fragment explosive access tool |
| FR2896577A1 (en) * | 2006-01-24 | 2007-07-27 | Giat Ind Sa | STARTING DEVICE FOR MULTI-MODE LOAD |
| WO2010066752A1 (en) * | 2008-12-12 | 2010-06-17 | Tda Armements S.A.S | Low-vulnerability pyrotechnical charge |
| CN102778181A (en) * | 2012-07-24 | 2012-11-14 | 西北核技术研究所 | Ultra-fast closing device for implosion compression pipeline |
| CN102927868A (en) * | 2012-11-23 | 2013-02-13 | 中国船舶重工集团公司第七〇五研究所 | Detonation wave form control device |
| US8402892B1 (en) | 2010-12-30 | 2013-03-26 | The United States Of America As Represented By The Secretary Of The Navy | Simultaneous nonelectric priming assembly and method |
| DE19540863B3 (en) * | 1995-11-02 | 2013-12-05 | Nexter Munitions | Ignition apparatus installed in warhead of e.g. rocket, has trigger units that enables simultaneous activation of relay charge unit to ensure triggering of explosive apparatus so that shock waves are generated in explosive apparatus |
| RU2524409C1 (en) * | 2013-04-11 | 2014-07-27 | Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом"-Госкорпорация "Росатом" | Explosive device |
| RU2531678C1 (en) * | 2013-07-26 | 2014-10-27 | Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" - Госкорпорация "Росатом" | Device for formation of blast wave in explosive charge |
| RU2553615C1 (en) * | 2014-01-30 | 2015-06-20 | Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом"-Госкорпорация "Росатом" | Explosive device |
| US9303966B1 (en) | 2015-01-29 | 2016-04-05 | The United States Of America As Represented By The Secretary Of The Navy | Symmetical initiation distributor for use in explosive detonation trains with an offset orientation |
| RU2628115C1 (en) * | 2016-06-20 | 2017-08-15 | Федеральное государственное унитарное предприятие "Российский Федеральный ядерный центр - Всероссийский научно-исследовательский институт экспериментальной физики" (ФГУП "РФЯЦ-ВНИИЭФ") | Detonation wave formation device |
| US9738568B1 (en) * | 2016-03-18 | 2017-08-22 | Goodrich Corporation | Methods and systems for an explosive cord |
| US9816792B1 (en) * | 2013-03-14 | 2017-11-14 | Spectre Materials Sciences, Inc. | Layered energetic material having multiple ignition points |
| US10254090B1 (en) | 2013-03-14 | 2019-04-09 | University Of Central Florida Research Foundation | Layered energetic material having multiple ignition points |
| US11060831B1 (en) * | 2020-05-14 | 2021-07-13 | The United States Of America As Represented By The Secretary Of The Army | System and method for routing flame within an explosive device |
| US11112222B2 (en) | 2019-01-21 | 2021-09-07 | Spectre Materials Sciences, Inc. | Propellant with pattern-controlled burn rate |
| US20220011079A1 (en) * | 2018-11-20 | 2022-01-13 | Saab Bofors Dynamics Switzerland Ltd. | Warhead with asymmetric initiation |
| US11650037B2 (en) | 2021-02-16 | 2023-05-16 | Spectre Materials Sciences, Inc. | Primer for firearms and other munitions |
| US12234198B2 (en) | 2020-08-05 | 2025-02-25 | Spectre Enterprises, Inc. | Passivated fuel |
| US12385727B2 (en) | 2023-04-29 | 2025-08-12 | Spectre Primer Technologies, Inc. | Fuzzy interface layer for thermite and primer made from thermite with fuzzy layer |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3016831A (en) * | 1958-10-02 | 1962-01-16 | Du Pont | Surface wave generator |
| US3311055A (en) * | 1965-04-23 | 1967-03-28 | Jr Richard H Stresau | Toroidal booster with cylindrically symmetrical output |
| US3430563A (en) * | 1963-08-07 | 1969-03-04 | Us Navy | Flexible detonation wave shaping device |
-
1970
- 1970-09-22 US US083260A patent/US3896731A/en not_active Expired - Lifetime
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3016831A (en) * | 1958-10-02 | 1962-01-16 | Du Pont | Surface wave generator |
| US3430563A (en) * | 1963-08-07 | 1969-03-04 | Us Navy | Flexible detonation wave shaping device |
| US3311055A (en) * | 1965-04-23 | 1967-03-28 | Jr Richard H Stresau | Toroidal booster with cylindrically symmetrical output |
Cited By (46)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4282814A (en) * | 1974-12-20 | 1981-08-11 | The United States Of America As Represented By The Secretary Of The Navy | Dual-end warhead initiation system |
| US4145972A (en) * | 1976-12-17 | 1979-03-27 | The United States Of America As Represented By The Secretary Of The Navy | Dual-mode warhead initiation system |
| EP0030189A1 (en) * | 1979-12-03 | 1981-06-10 | Aerospatiale Societe Nationale Industrielle | Multiway connector and process for transmitting pyrotechnical signals |
| US4404910A (en) * | 1979-12-03 | 1983-09-20 | Societe Nationale Industrielle Aerospatiale | Multichannel connection and method for transmitting pyrotechnic orders |
| US4475461A (en) * | 1981-06-17 | 1984-10-09 | The United States Of America As Represented By The Secretary Of The Navy | Monolithic multi-point warhead initiator |
| US4499828A (en) * | 1983-06-01 | 1985-02-19 | The United States Of America As Represented By The United States Department Of Energy | Barrier breaching device |
| DE3503013C1 (en) * | 1985-01-30 | 1986-06-26 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Safety device |
| FR2601126A1 (en) * | 1986-07-03 | 1988-01-08 | Matra Manurhin Defense | Primer pyrotechnic chain with shutter |
| US4784062A (en) * | 1986-07-31 | 1988-11-15 | Diehl Gmbh & Co. | Fuze for a projectile-forming charge |
| US4899663A (en) * | 1989-02-15 | 1990-02-13 | Automotive Systems Laboratory, Inc. | Percussion initiated inflator assembly |
| DE19540863B3 (en) * | 1995-11-02 | 2013-12-05 | Nexter Munitions | Ignition apparatus installed in warhead of e.g. rocket, has trigger units that enables simultaneous activation of relay charge unit to ensure triggering of explosive apparatus so that shock waves are generated in explosive apparatus |
| RU2203260C2 (en) * | 1996-01-11 | 2003-04-27 | Дзе Энсайн-Бикфорд Компани | Detonators having inputs with many lines |
| US6220166B1 (en) * | 1999-08-02 | 2001-04-24 | Sandia Corporation | Apparatus and method for producing fragment-free openings |
| RU2226254C2 (en) * | 2002-04-22 | 2004-03-27 | Российский Федеральный Ядерный Центр - Всероссийский Научно-Исследовательский Институт Экспериментальной Физики | Device for forming explosion wave |
| US6817297B1 (en) * | 2003-01-09 | 2004-11-16 | The United States Of America As Represented By The Secretary Of The Navy | Low-cost, no-fragment explosive access tool |
| US6865990B1 (en) * | 2003-01-09 | 2005-03-15 | The United States Of America As Represented By The Secretary Of The Navy | Low-cost, no-fragment explosive access tool |
| US6966263B1 (en) * | 2003-01-09 | 2005-11-22 | The United States Of America As Represented By The Secretary Of The Navy | Low-cost, no-fragment explosive access tool for soft metal containers |
| FR2896577A1 (en) * | 2006-01-24 | 2007-07-27 | Giat Ind Sa | STARTING DEVICE FOR MULTI-MODE LOAD |
| US8479653B2 (en) | 2008-12-12 | 2013-07-09 | Tda Armements Sas | Low-vulnerability pyrotechnical charge |
| FR2939881A1 (en) * | 2008-12-12 | 2010-06-18 | Tda Armements Sas | PYROTECHNIC LOAD WITH LOW VULNERABILITY |
| AU2009326087B2 (en) * | 2008-12-12 | 2015-04-02 | Tda Armements S.A.S. | Low-vulnerability pyrotechnical charge |
| WO2010066752A1 (en) * | 2008-12-12 | 2010-06-17 | Tda Armements S.A.S | Low-vulnerability pyrotechnical charge |
| US8973502B2 (en) | 2010-12-30 | 2015-03-10 | The United States Of America As Represented By The Secretary Of The Navy | Simultaneous nonelectric priming assembly and method |
| US8402892B1 (en) | 2010-12-30 | 2013-03-26 | The United States Of America As Represented By The Secretary Of The Navy | Simultaneous nonelectric priming assembly and method |
| CN102778181B (en) * | 2012-07-24 | 2014-09-17 | 西北核技术研究所 | Ultra-fast closing device for implosion compression pipeline |
| CN102778181A (en) * | 2012-07-24 | 2012-11-14 | 西北核技术研究所 | Ultra-fast closing device for implosion compression pipeline |
| CN102927868B (en) * | 2012-11-23 | 2014-11-19 | 中国船舶重工集团公司第七〇五研究所 | Detonation wave form control device |
| CN102927868A (en) * | 2012-11-23 | 2013-02-13 | 中国船舶重工集团公司第七〇五研究所 | Detonation wave form control device |
| US9816792B1 (en) * | 2013-03-14 | 2017-11-14 | Spectre Materials Sciences, Inc. | Layered energetic material having multiple ignition points |
| US10254090B1 (en) | 2013-03-14 | 2019-04-09 | University Of Central Florida Research Foundation | Layered energetic material having multiple ignition points |
| RU2524409C1 (en) * | 2013-04-11 | 2014-07-27 | Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом"-Госкорпорация "Росатом" | Explosive device |
| RU2531678C1 (en) * | 2013-07-26 | 2014-10-27 | Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" - Госкорпорация "Росатом" | Device for formation of blast wave in explosive charge |
| RU2553615C1 (en) * | 2014-01-30 | 2015-06-20 | Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом"-Госкорпорация "Росатом" | Explosive device |
| US9303966B1 (en) | 2015-01-29 | 2016-04-05 | The United States Of America As Represented By The Secretary Of The Navy | Symmetical initiation distributor for use in explosive detonation trains with an offset orientation |
| US9738568B1 (en) * | 2016-03-18 | 2017-08-22 | Goodrich Corporation | Methods and systems for an explosive cord |
| US10087119B2 (en) * | 2016-03-18 | 2018-10-02 | Goodrich Corporation | Methods and systems for an explosive cord |
| US20200024212A1 (en) * | 2016-03-18 | 2020-01-23 | Goodrich Corporation | Methods and systems for an explosive cord |
| US10793486B2 (en) * | 2016-03-18 | 2020-10-06 | Goodrich Corporation | Methods and systems for an explosive cord |
| RU2628115C1 (en) * | 2016-06-20 | 2017-08-15 | Федеральное государственное унитарное предприятие "Российский Федеральный ядерный центр - Всероссийский научно-исследовательский институт экспериментальной физики" (ФГУП "РФЯЦ-ВНИИЭФ") | Detonation wave formation device |
| US20220011079A1 (en) * | 2018-11-20 | 2022-01-13 | Saab Bofors Dynamics Switzerland Ltd. | Warhead with asymmetric initiation |
| US11965720B2 (en) * | 2018-11-20 | 2024-04-23 | Saab Bofors Dynamics Switzerland Ltd. | Warhead with asymmetric initiation |
| US11112222B2 (en) | 2019-01-21 | 2021-09-07 | Spectre Materials Sciences, Inc. | Propellant with pattern-controlled burn rate |
| US11060831B1 (en) * | 2020-05-14 | 2021-07-13 | The United States Of America As Represented By The Secretary Of The Army | System and method for routing flame within an explosive device |
| US12234198B2 (en) | 2020-08-05 | 2025-02-25 | Spectre Enterprises, Inc. | Passivated fuel |
| US11650037B2 (en) | 2021-02-16 | 2023-05-16 | Spectre Materials Sciences, Inc. | Primer for firearms and other munitions |
| US12385727B2 (en) | 2023-04-29 | 2025-08-12 | Spectre Primer Technologies, Inc. | Fuzzy interface layer for thermite and primer made from thermite with fuzzy layer |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US3896731A (en) | Explosive initiator device | |
| US3853059A (en) | Configured blast fragmentation warhead | |
| US3430563A (en) | Flexible detonation wave shaping device | |
| US6158347A (en) | Detonator | |
| US3565009A (en) | Aimed quadrant warhead | |
| FI57741C (en) | ANORDINATION FOER INITIERING AV SPRAENGLADDNINGAR | |
| US3461801A (en) | Multi-canister ejecting device | |
| GB1434034A (en) | Method and equipment for forming a single cloud of radar reflecting chaff within the atmosphere | |
| US4145972A (en) | Dual-mode warhead initiation system | |
| US3703865A (en) | Electronically controlled aimed blast warhead | |
| US4392432A (en) | Air burst munitions simulator | |
| US2981186A (en) | Electric detonator | |
| US3714897A (en) | Directed warhead | |
| US3211097A (en) | Pyrogen squib | |
| US3373686A (en) | Explosive actuator | |
| US4579059A (en) | Tubular projectile having an explosive material therein | |
| US4282814A (en) | Dual-end warhead initiation system | |
| US5144893A (en) | Safe ordnance initiation system | |
| US3664262A (en) | Reactive focusing warhead concept | |
| US3720168A (en) | Elliptical warhead | |
| US5293821A (en) | Delay initiator for blasting | |
| US5221810A (en) | Embedded can booster | |
| US3618523A (en) | Stab-electric detonator | |
| US3311055A (en) | Toroidal booster with cylindrically symmetrical output | |
| US4348958A (en) | Projectile having impact responsive initiator means |