US1810000A - Booster - Google Patents
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- Publication number
- US1810000A US1810000A US475745A US47574521A US1810000A US 1810000 A US1810000 A US 1810000A US 475745 A US475745 A US 475745A US 47574521 A US47574521 A US 47574521A US 1810000 A US1810000 A US 1810000A
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- Prior art keywords
- booster
- charge
- cavity
- detonator
- shell
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/201—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class
- F42B12/204—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class for attacking structures, e.g. specific buildings or fortifications, ships or vehicles
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- 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
Definitions
- the subject of this invention is a booster intended for use in exploding shells, bombs, grenades, torpedoes and other articles of ammunition, and in blasting explosives. It is particularly adapted for use in detonating high explosives but its principles are equally applicable to explosives of a low order.
- the booster casing is usuall composed of a drawn, pressed or. machined metal cup.
- the thickness of the walls and the interior shape of the cavity is determined chiefiy by considerations of manufacture rather than by scientific analysis of the practice involved in securing a maximum desired effect of the booster.
- any type of booster for each particular type of shell and the amount of explosive contained in any type of booster is sufficient to cause detonation in the shell charge when the initiating charge (the detonator) is preponderant in size and strength, and the shell charge is in immediate contact with the booster casing. It is possible to obtain the first condition when the element of danger in having an excessively large charge of fulminate of mercury is disregarded or when mechanical means for separating the detonator from the booster charge is provided, but even so, the less fulminate contained in a fuse the less is the element of danger.
- the Walls of the casing are of immaterialthickness, the determining factor being easiness of manufacture and strength sufficient to carry the load during the period of acceleration.
- the size of the casing is usually determined by experiments When ex lesion of the booster takes place the walls Being relatively thin and of more or less uniform thickness, the force of explosion is expended equally in all directions. The total ener thus transferred to the shell is distribu over a relatively large surface and unless the energy per unit of surface is sufliciently great to initiate a sympathetic detonating wave in the charge a low order of detonation must result.
- the presence of an air gap around ordinary cup boosters is considered detrimental to the transmission of detonation from the booster to the shell charge, even though the booster be completely surrounded by the charge.
- As an air space of varying dimensions is inevitable due to the necessary tolerances in manufacture and loading, all boosters of the ordinary type are necessarily less effective under actual conditions than in ideal conditions.
- the detonation in the booster was originated at or near the center of the base of the cup or in the con'ic section forms nearthe focus of the form. This method of originating the detonation is to be preferred over other methods. An improvement in the position of the detonator was also found. Ordinarily a detonator is counter-sunk in the main booster charge so that it is surrounded by the booster. This is objectionable, however, on account of the amount of metal which must necessarily exist between the detonator and the charge itself, on account of assembling methods.
- the detonator since the detonator is not highly confined, the force of detonation occurs equally in all directions and consequently the charge must be of sufficient strength to produce the required energy per unit area to initiate the detonation in the booster charge. I have found that if the detonator is removed from The advantage in using this type of detonator may be found in the additional safety, economy, and eiiiciency afforded.
- FIG. 1 is a View in longitudinal section of an ordinary form of booster, the shell in which the booster is secured being shown in broken lines;
- Fig. 2 is an enlarged view in longitudinal section of the booster, the dispersion of the force of explosion thereof being represented by arrows;
- Fig. 3 is a view in longitudinal section of a booster constructed in accordance with my invention.
- Fig. 4 is an enlarged view of the same, a fragment of the shell to which it is secured being shown and a modified form of detonator casing also being shown;
- 1 refers to a shell body having a cavity 2 for the reception of the charge of high explosive in the end of which shell is threaded an ordinary booster casing 3, containing the booster charge 4 in which is countersunk the detonator 5 inclosed in a suitable detonator casing comprising the containers and holders 9, and 11.
- the booster has connected thereto the usual form of fuse 7 which Operates to fire or 8 refers to the usual air gap between the booster casing and the explosive charge in the shell while the dotted line 6 indicates the air gap as the same would appear after set back of the charge upon firing of the shell from the gun.
- Fig. 2 the series of dotted arrows indicate the dispersion of the force of explosion of the detonator while the solid arrows indicate the dispersion of the force of explosion of the booster charge, showing that in the ordinary form of booster the energy generated by the explosion of the charge is dispersed over a large area of the explosive in the shell thereby diminishing the force upon a unit area.
- a typical boost-er constructed in accordance with my invention is shown.
- the booster casing 12 is formed with thick heavy walls 13 which surround the booster cavity in which is contained the booster charge 14.
- the booster casing is centrally bored, such bore communicating with the cavity and being adapted to receive the cord of explosive 15 which may be the same explosive material as that filling the booster cavity.
- the casing may be ccunter-sunk to receive a detonator casing 17 which is centrally bored for the reception of As shown in Fig. 4, the bore for the reception of the detonator 16 may be formed directly in the booster casing 12 thus obviating the necessity for the extra piece 17.
- a thin metal'cap 18 may be secured in any suitable manner over the end of the booster casing 12 for the purpose of closing the cavity, retaining the booster charge in place and excluding moisture therefrom.
- the usual air gap is indicated by the reference numeral 8 in Fig. 4 and the increase of this air of a cylinder; Fig. 9 one in the form of a hemisphere and Fig. 10 a cavity composed of superimposed cylinders.
- the cylinder shown in Fig. 8 is very efficient when surrounded with strong walls, and is a preferred form in boosters not requiring the highest eiiiciency.
- Means for increasing the eflectiveness of booster charges embodying, a strong walled container having a cavity therein, the walls of which gradually converge toward the bottom, a detonator located in the strong Walled container and remote from the booster cavity and a cord of explosive connecting'the detonator and booster cavity.
- Means for increasing the eifectiveness of booster charges embodying, a strong walled container having a cavity therein, the walls of which gradually converge toward the bottom, adetonator located in the strong "walled container remote from the booster cavity, a cord of explosive connecting the detonator and booster cavity located so as to direct the initiation of detonation in the booster charge along the axial line of the booster cavity.
- detonator located in the strong Walled container and remote from the booster cavity and means for communicating the wave of detonation from the detonator to the booster cavity.
- Means for increasing the effectiveness of booster charges embodying, a strong walled container having a booster cavity therein, a detonator located in the strong walled container and remote from the booster cavity and means for communicating the Wave of detonation from the detonator to the booster cavity along the axial line of said cavity.
- Means for increasing the effectiveness of booster charges embodying, a strong walled container having a cavity therein, the walls of which gradually converge toward the bottom, a detonator located in the strong walled container remote from the booster cavity and communicating means between the detonator and the booster cavity whereby the wave of detonation from the detonator Will be communicated to the booster cavity.
- a detonating fuse comprising a body in one end of which is a chamber for the booster charge, the walls of such chamber converging at the rear inner end thereof so as to close the cavity except for a channel of detonation, and being of a curvature to direct the waves of detonating force, produced by detonation of the booster charge, forwardly'and into the bursting charge of the shell to which the fuse is applied and, automatically operating means for detonating the'booster charge.
- a detonating fuse coniprising, a body in one end of which is a chamber for the booster charge, the walls of which chamber converge B at the rear, so as to close the chamber except for a channel of detonation leading to the chamber and, being curved to direct and concentrate the waves of detonating force, pro- 5 quizd by the detonation of the booster charge, into the bursting charge of the shell to which the fuse is applied.
- a detonating fuse comprising, a body in one end of which is 'a chamber for a detonating charge, the walls of which chamber converge at the rear so as to close the chamber except for a channelthrough which the charge may be detonated, and being of a curvature to direct the resulting waves of detonating force forwardly and out of the chamber.
- a detonating fuse comprising a body in one end of which is a chamber for a detonating charge, the walls of which chamber converge at the rear so as to close the chamber except for a channel through which the charge may be detonated, and being of a curvature to reflect and concentrate the resulting waves of detonating forceforwardly and out of the chamber.
- a detonating fuse comprisin a body in one end of which is a chamber fora%etonating charge, the walls of 'suchchamber being of ellipsoidalcurvature.
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Description
June 16, 1931. J. H. WOODBERRY BOOSTER Filed June 7, 1921 2 Sheets-Sheet 1 INVENT June 1931.
J. H. wooDE Y" BOOSTER 2' Sheets-Sheet 2 Filed June 7, 1921 INVENTOR.
, ment for governmental purposes. without the Patented June 16, 1931 UNITED STATES PATENT OFFICE JOHN H. WOODBERBY, OF THE UNITED STATES ARMY, FRANKFORD ARSENAL, BRIDESBURQ, PENNSYLVANIA BOOSTER Application filed June 7, 1921. Serial No. 475,745.
(GRANTED UNDER THE ACT OF MARCH 8, 1888, AS AMENDED APRIL 30, 1928; 370 0. G. 757) The invention described herein may be manufactured and usedby or for the Governpayment to me of any royalty thereon.
The subject of this invention is a booster intended for use in exploding shells, bombs, grenades, torpedoes and other articles of ammunition, and in blasting explosives. It is particularly adapted for use in detonating high explosives but its principles are equally applicable to explosives of a low order.
A form of the present invention wherein explosive charges are controlled is shown in my Patents 1,376,908 and 1,462,313, applications for which were filed December 10, 1918.
To fully show the principles involved in my invention and to better illustrate its ob jects and uses, its use as applied to high explosive artillery shells will be here described sufiiciently to explain its typical action.
In order to roduce a detonation with high explosive shel s, that is in shells loaded with explosives such as T. N. T., tetrylfamatol, picric acid, and the like, two conditions must obtain: First there must be a mechanical means for initiating the explosive, and, second, there must be means whereby this initial explosion will be accelerated and augmented until suflicient energy in the form of highly heated and highly compressed gas has been obtained to produce a sympathetic detonation of the shell charge. The first condition is obtained by means of a fuse which contains usually a rimer and fulminate detonator.
In any ut the minor caliber shells it has been found that the fulminate detonator of itself is not usually suflicient to produce the necessary energy to cause the shell charge to detonate without assistance. Consequently, it is necessary to augment this fulminate charge with an auxiliary charge of owerful yet easily detonated explosive.- T 's additional explosive is commonly known as a booster charge and the container of this charge is a booster casing.
In common practice the booster casing is usuall composed of a drawn, pressed or. machined metal cup. The thickness of the walls and the interior shape of the cavity is determined chiefiy by considerations of manufacture rather than by scientific analysis of the practice involved in securing a maximum desired effect of the booster.
for each particular type of shell and the amount of explosive contained in any type of booster is sufficient to cause detonation in the shell charge when the initiating charge (the detonator) is preponderant in size and strength, and the shell charge is in immediate contact with the booster casing. It is possible to obtain the first condition when the element of danger in having an excessively large charge of fulminate of mercury is disregarded or when mechanical means for separating the detonator from the booster charge is provided, but even so, the less fulminate contained in a fuse the less is the element of danger. It is seldom possible, however, to have the second condition prevail in actual practice for even though the shell charge is loaded in intimate contact with the booster casing in high velocity shells, the inertia of the shell is enormous, and the resulting set back force, due to linear acceleration in the bore is usually sufficient to further compress the shell charge and therefore produce an air gapg in the nose of the shell. This being the location of the booster in point fused shells, will result in a cavity surrounding. at least a portion of the booster casing. A quantity of the energy of the booster 1s, therefore, entirely lost in its direct detonating effect and its power is so diminished that a low order of detonation in the shell or complete failure must result. To overcome this condition, the common practice has been to providea booster charge much in excess of that actually required to detonate a shell under ideal conditions. The failure to present sufiicient energy to the shell charge to initiate the breaking down of the molecularstructure of the charge to its most effective form must result unsatisfactorily.
In boosters now in common use, the Walls of the casing are of immaterialthickness, the determining factor being easiness of manufacture and strength sufficient to carry the load during the period of acceleration.
The size of the casing is usually determined by experiments When ex lesion of the booster takes place the walls Being relatively thin and of more or less uniform thickness, the force of explosion is expended equally in all directions. The total ener thus transferred to the shell is distribu over a relatively large surface and unless the energy per unit of surface is sufliciently great to initiate a sympathetic detonating wave in the charge a low order of detonation must result. The presence of an air gap around ordinary cup boosters is considered detrimental to the transmission of detonation from the booster to the shell charge, even though the booster be completely surrounded by the charge. As an air space of varying dimensions is inevitable due to the necessary tolerances in manufacture and loading, all boosters of the ordinary type are necessarily less effective under actual conditions than in ideal conditions.
Bearing these, and other inherent weaknesses of existing boosters in mind, I inane gurated a series of experiments to develop a booster of more efficiency by eliminating or minimizing the above mentioned defects and by providing some logical means of initiating the detonation in the booster itself. My experiments were made in an attempt to direct the entire eflective force of the booster toward one point in the shell charge, in much the same manner as light waves may be controlled and directed. In carrying out these experiments I found that the force of explosion at the mouth of a cup containing explosives is much greater when the cup was not ruptured than when the cup was lown to pieces and that when the cup was ruptured the force of explosion varied directly with.
the thickness of the wall. It was, therefore, concluded that a booster made of strong metal and having thick walls to prevent equal expansion of the gases in all directions and so constructed as to cause the gases to flow in the desired direction thereby giving a concentrated explosive effect, would be of more value than thin walled boosters such as are now in use.
Furthermore I found that better results were obtained when the mouth of the cup was obstructed less, hence I concluded that a thick wall booster should be sealed only sufficiently to hold the explosive in place and to prevent undue exposure to moisture, etc. I found furthermore that in the thick wall cup the force of explosion was also dependent upon the interior shape of the cup, the detonating effect being greatest in an ellipsodial cavity, and diminishing in the other paraboloidal, cylindrical, and conoidal. It is, therefore, concluded that a booster having a cavity whose vertical section is a conic section and particularly an ellipse is to be preferred. One exception is to be noted, however, and that is that a cylindrical cavity isbetter than a conoidal cavity. Obviously any form approximating the above true curves'will give ap roximate results. I
n all of the above experiments the detonation in the booster was originated at or near the center of the base of the cup or in the con'ic section forms nearthe focus of the form. This method of originating the detonation is to be preferred over other methods. An improvement in the position of the detonator was also found. Ordinarily a detonator is counter-sunk in the main booster charge so that it is surrounded by the booster. This is objectionable, however, on account of the amount of metal which must necessarily exist between the detonator and the charge itself, on account of assembling methods. Furthermore, since the detonator is not highly confined, the force of detonation occurs equally in all directions and consequently the charge must be of sufficient strength to produce the required energy per unit area to initiate the detonation in the booster charge. I have found that if the detonator is removed from The advantage in using this type of detonator may be found in the additional safety, economy, and eiiiciency afforded.
With these and other objects in view the invention resides in the novel arrangement and combination of parts and in the details of construction hereinafter described and claimed, it being understood that changes in the precise embodiment of the invention herein disclosed may be made within the scope of what is claimed without departing from the spirit of the invention.
Practical embodiments of the invention are shown in the accompanying drawings wherein Fig. 1 is a View in longitudinal section of an ordinary form of booster, the shell in which the booster is secured being shown in broken lines;
Fig. 2 is an enlarged view in longitudinal section of the booster, the dispersion of the force of explosion thereof being represented by arrows;
Fig. 3 is a view in longitudinal section of a booster constructed in accordance with my invention;
Fig. 4 is an enlarged view of the same, a fragment of the shell to which it is secured being shown and a modified form of detonator casing also being shown;
' the detonator 16.
, detonate the detonator.
cavities.
Referring to the drawings by numerals of reference, 1 refers to a shell body having a cavity 2 for the reception of the charge of high explosive in the end of which shell is threaded an ordinary booster casing 3, containing the booster charge 4 in which is countersunk the detonator 5 inclosed in a suitable detonator casing comprising the containers and holders 9, and 11.
The booster has connected thereto the usual form of fuse 7 which Operates to fire or 8 refers to the usual air gap between the booster casing and the explosive charge in the shell while the dotted line 6 indicates the air gap as the same would appear after set back of the charge upon firing of the shell from the gun.
In Fig. 2 the series of dotted arrows indicate the dispersion of the force of explosion of the detonator while the solid arrows indicate the dispersion of the force of explosion of the booster charge, showing that in the ordinary form of booster the energy generated by the explosion of the charge is dispersed over a large area of the explosive in the shell thereby diminishing the force upon a unit area.
Referring to Figs. 3 and 4 a typical boost-er constructed in accordance with my invention is shown. .In these figures the booster casing 12 is formed with thick heavy walls 13 which surround the booster cavity in which is contained the booster charge 14. .The booster casing is centrally bored, such bore communicating with the cavity and being adapted to receive the cord of explosive 15 which may be the same explosive material as that filling the booster cavity. The casing may be ccunter-sunk to receive a detonator casing 17 which is centrally bored for the reception of As shown in Fig. 4, the bore for the reception of the detonator 16 may be formed directly in the booster casing 12 thus obviating the necessity for the extra piece 17.
A thin metal'cap 18 may be secured in any suitable manner over the end of the booster casing 12 for the purpose of closing the cavity, retaining the booster charge in place and excluding moisture therefrom. The usual air gap is indicated by the reference numeral 8 in Fig. 4 and the increase of this air of a cylinder; Fig. 9 one in the form of a hemisphere and Fig. 10 a cavity composed of superimposed cylinders. The cylinder shown in Fig. 8 is very efficient when surrounded with strong walls, and is a preferred form in boosters not requiring the highest eiiiciency.
Having described by invention what I claim is:
1. Means for increasing the eflectiveness of booster charges embodying, a strong walled container having a cavity therein, the walls of which gradually converge toward the bottom, a detonator located in the strong Walled container and remote from the booster cavity and a cord of explosive connecting'the detonator and booster cavity.
2. Means for increasing the eifectiveness of booster charges embodying, a strong walled container having a cavity therein, the walls of which gradually converge toward the bottom, adetonator located in the strong "walled container remote from the booster cavity, a cord of explosive connecting the detonator and booster cavity located so as to direct the initiation of detonation in the booster charge along the axial line of the booster cavity.
3. Means for increasing the effectiveness of booster-charges embodying, a strong walled container having a booster cavity therein, av
detonator located in the strong Walled container and remote from the booster cavity and means for communicating the wave of detonation from the detonator to the booster cavity.
4. Means for increasing the effectiveness of booster charges embodying, a strong walled container having a booster cavity therein, a detonator located in the strong walled container and remote from the booster cavity and means for communicating the Wave of detonation from the detonator to the booster cavity along the axial line of said cavity.
5. Means for increasing the effectiveness of booster charges embodying, a strong walled container having a cavity therein, the walls of which gradually converge toward the bottom, a detonator located in the strong walled container remote from the booster cavity and communicating means between the detonator and the booster cavity whereby the wave of detonation from the detonator Will be communicated to the booster cavity.
6. A detonating fuse comprising a body in one end of which is a chamber for the booster charge, the walls of such chamber converging at the rear inner end thereof so as to close the cavity except for a channel of detonation, and being of a curvature to direct the waves of detonating force, produced by detonation of the booster charge, forwardly'and into the bursting charge of the shell to which the fuse is applied and, automatically operating means for detonating the'booster charge.
7. A detonating fuse coniprising, a body in one end of which is a chamber for the booster charge, the walls of which chamber converge B at the rear, so as to close the chamber except for a channel of detonation leading to the chamber and, being curved to direct and concentrate the waves of detonating force, pro- 5 duced by the detonation of the booster charge, into the bursting charge of the shell to which the fuse is applied.
8. A detonating fuse comprising, a body in one end of which is 'a chamber for a detonating charge, the walls of which chamber converge at the rear so as to close the chamber except for a channelthrough which the charge may be detonated, and being of a curvature to direct the resulting waves of detonating force forwardly and out of the chamber.
9. A detonating fuse comprising a body in one end of which is a chamber for a detonating charge, the walls of which chamber converge at the rear so as to close the chamber except for a channel through which the charge may be detonated, and being of a curvature to reflect and concentrate the resulting waves of detonating forceforwardly and out of the chamber.
10. A detonating fuse comprisin a body in one end of which is a chamber fora%etonating charge, the walls of 'suchchamber being of ellipsoidalcurvature.
JOHN HYWOODBERRY. Y
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US475745A US1810000A (en) | 1921-06-07 | 1921-06-07 | Booster |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US475745A US1810000A (en) | 1921-06-07 | 1921-06-07 | Booster |
Publications (1)
Publication Number | Publication Date |
---|---|
US1810000A true US1810000A (en) | 1931-06-16 |
Family
ID=23888927
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US475745A Expired - Lifetime US1810000A (en) | 1921-06-07 | 1921-06-07 | Booster |
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US (1) | US1810000A (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2513233A (en) * | 1949-03-15 | 1950-06-27 | Laud Stanley Byers | Multiple jet blasting charge |
US2882822A (en) * | 1944-01-05 | 1959-04-21 | Clarence B Crane | Fuze housing |
US3234875A (en) * | 1964-01-09 | 1966-02-15 | Eugene O Tolson | Jet perforating apparatus |
US3238872A (en) * | 1964-02-10 | 1966-03-08 | Aerojet General Co | Shaped charge construction |
US3320889A (en) * | 1965-02-12 | 1967-05-23 | Aerojet General Co | Detonation initiator |
US3893395A (en) * | 1965-07-26 | 1975-07-08 | Us Navy | End coupler for heat resistant mild detonating fuse |
FR2436961A1 (en) * | 1978-09-22 | 1980-04-18 | Sarmac Sa | EXPLOSIVE RIFLE GRENADE |
DE3000413A1 (en) * | 1979-01-12 | 1980-07-31 | Raufoss Ammunisjonsfabrikker | DETONATION ELEMENT |
EP0015697A1 (en) * | 1979-02-26 | 1980-09-17 | E.I. Du Pont De Nemours And Company | Non-electric delay detonator and assembly of a detonating cord and a delay detonator |
EP0149179A2 (en) * | 1984-01-18 | 1985-07-24 | DIEHL GMBH & CO. | Projectile |
WO2008105924A2 (en) | 2006-08-29 | 2008-09-04 | Raytheon Company | Warhead booster explosive lens |
-
1921
- 1921-06-07 US US475745A patent/US1810000A/en not_active Expired - Lifetime
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2882822A (en) * | 1944-01-05 | 1959-04-21 | Clarence B Crane | Fuze housing |
US2513233A (en) * | 1949-03-15 | 1950-06-27 | Laud Stanley Byers | Multiple jet blasting charge |
US3234875A (en) * | 1964-01-09 | 1966-02-15 | Eugene O Tolson | Jet perforating apparatus |
US3238872A (en) * | 1964-02-10 | 1966-03-08 | Aerojet General Co | Shaped charge construction |
US3320889A (en) * | 1965-02-12 | 1967-05-23 | Aerojet General Co | Detonation initiator |
US3893395A (en) * | 1965-07-26 | 1975-07-08 | Us Navy | End coupler for heat resistant mild detonating fuse |
FR2436961A1 (en) * | 1978-09-22 | 1980-04-18 | Sarmac Sa | EXPLOSIVE RIFLE GRENADE |
DE3000413A1 (en) * | 1979-01-12 | 1980-07-31 | Raufoss Ammunisjonsfabrikker | DETONATION ELEMENT |
EP0015697A1 (en) * | 1979-02-26 | 1980-09-17 | E.I. Du Pont De Nemours And Company | Non-electric delay detonator and assembly of a detonating cord and a delay detonator |
EP0149179A2 (en) * | 1984-01-18 | 1985-07-24 | DIEHL GMBH & CO. | Projectile |
EP0149179A3 (en) * | 1984-01-18 | 1985-08-14 | Diehl Gmbh & Co. | Projectile |
WO2008105924A2 (en) | 2006-08-29 | 2008-09-04 | Raytheon Company | Warhead booster explosive lens |
EP2057437A2 (en) * | 2006-08-29 | 2009-05-13 | Raytheon Company | Warhead booster explosive lens |
EP2057437A4 (en) * | 2006-08-29 | 2013-01-02 | Raytheon Co | Warhead booster explosive lens |
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