US3109369A - Disposal of encased explosives - Google Patents

Disposal of encased explosives Download PDF

Info

Publication number
US3109369A
US3109369A US538173A US53817344A US3109369A US 3109369 A US3109369 A US 3109369A US 538173 A US538173 A US 538173A US 53817344 A US53817344 A US 53817344A US 3109369 A US3109369 A US 3109369A
Authority
US
United States
Prior art keywords
explosive
charge
housing
thermit
reaction
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
Application number
US538173A
Inventor
Harold J Plumley
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US538173A priority Critical patent/US3109369A/en
Priority to US353692A priority patent/US3054349A/en
Application granted granted Critical
Publication of US3109369A publication Critical patent/US3109369A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B3/00Blasting cartridges, i.e. case and explosive
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63GOFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
    • B63G7/00Mine-sweeping; Vessels characterised thereby
    • B63G7/02Mine-sweeping means, Means for destroying mines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B33/00Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
    • F42B33/06Dismantling fuzes, cartridges, projectiles, missiles, rockets or bombs

Definitions

  • This invention relates to the disposal of explosive-bearing ordnance by techniques involving either a simple burning of the explosive charge in fair, the necessary oxygen being supplied by the air, and/or by a self-sustaining reductive reaction requiring no air or oxygen supply, and which may accordingly be effected under water.
  • An important object of the invention is to provide improved means whereby the explosive charges of bombs, mines, depth charges rand other explosive-bearing ordnance may be removed in a quick, simple and eliicient manner, with the least possible risk of high Korder detonation.
  • Another object is to provide such means which requires, in order to effectuate the removal of the explosive charge, only relatively light, compact and easily portable apparatus, and which, further, involves the use of apparatus which may be operated from a safe distance and which may be set up Without creating such mechanical disturbance or magnetic etect as might initiate an unwanted detonation in event the ordnance should be equipped with anti-magnetic and/ or anti-disturbance devices or the like.
  • the present invention also includes among its objects, therefore, the overcoming of the indicated diliiculties, and the entirely safe destruction of explosive-bearing ordnance under tlhe diiiicult conditions outlined.
  • Another object of this invention is to provide such means involving a construction formed entirely of nonferrous materials, which may be loaded with non-magnetic Therrnit, so that danger of tiring a mine or other explosive device equipped with magnetically responsive elements is eliminated.
  • Another object is to provide such a mechanism which is capable of withstanding the great thermal shock involved in the rapid development of a thermal gradient of about 4000D F. across the wall thickness of .the unit, and the rapid cooling eifect of the surrounding water.
  • Another object is to provide such a mechanism having delay means adapted to prevent the release of the Thermit until approximately l5 seconds have elapsed after ignition of the charge, to insure that the Thermit reacts with reasonable completeness before such reaction is stopped by release of the molten iron.
  • Still another object is to provide electric ignition means, and to protect the electrical lead-in and other means lassociated therewith against the high pressures which may be involved and which may be applied from either or both sides.
  • FIGURE l is a perspective view of a mine to which is shown attached a preferred means for initiating self-destruction in accordance with the present invention
  • FIGURE 2 is a vertical, substantially diametric crosssection of the initiating device, taken substantially on the line 2 2 ⁇ of FIGURE l and looking in the direction of the arrow;
  • FEC-URE 3 is a sectional detail taken substantially on the line 3 3 of FXGURE 2 and looking in the direction of the arrow;
  • FIGURE 4 is a perspective v-iew of a bomb, together with rigging, and an initiating device supported by the rigging7 such devicve being or" somewhat modified construction;
  • FIGURE 5 is a vertical substantial-ly dametric sectional view taken substantially on the line 5 5 of FIGURE 4 and looking in the direction of the arrow;
  • FIGURE 6 is a vertical substantially diametric crosssectional view of a unit constructed in accordance with the present invention and suitable for underwater use, showing the same in position upon a mine case, which is fragmentarily illustrated;
  • FIGURE 7 is 'a view partly in top plan and partly in cross-section taken Isubstantially on the line 7 7 of FlGURE 6 and looking in the direction of the arrow.
  • a slow, selfdestructive reaction may be initiated under water as well as above ground, by exposing the charge to a temperature of about 2500" F. for a short time, and that furthermore, Ksuch self-destructive reaction will continue and spread throughout the charge, destroying it completely with no danger whatsoever of causing detionation of any part of the charge.
  • the essential feature of this reaction is apparently the progressive reduction of the nitrated organic constituents of the explosive by the metallic aluminum.
  • the solid end product is a porous ash, a typical sample of which has been found to be composed of 94% aluminum oxide and 6% carbon. Ammonia is prominent among the gaseous end products of the reaction.
  • non-violent self-destruction of explosives under water may be made to occur by ano-ther type of reaction which differs from the above described auto reduction in that it takes place in certain explosives which are entirely free of metall-ic reducing agents and the end products of which seem to be entirely gaseous, no ash whatever being left.
  • This reaction is apparently a slow exothermic decomposition started by local heating of the charge, and it progresses automatically due to the heat yield of the reaction.
  • the condition for the sub-surface auto-decomposition reaction in this manner is the presence in the explosive of either hexanitrodiphenylamine or cyclonite. This reaction also occurs Without violence and with a rate of gaseous discharge which is entirely mode-rate.
  • the case of the explosive-bearing ordnance is penetrated and charge ignition initiated, in a single operation, by allowing a pool or jet of molten iron, obtained from a Thermit reaction, to contact ⁇ or irnpinge upon the mine or bomb.
  • FIGURES 1, 2 and 3 show a suitable T hermit crucible adapted to be used in air, by placing the same upon the case of the item of ordnance to be depotentiated.
  • the Thermit may be fired from a distance by means of a squib which is electrically operable.
  • n-o magnetic materials are used in the construction of the crucible, and hematite base Thermit is used, since it is non-magnetic, unless it is certain that the mine or other ordnance is so designed that it is not sensitive to magnetic materials, in which event black magnetite base Thermit may be used, since it affords greater burning speed.
  • a unitary Thermit burning charge l is housed in a container formed of a cylindrical tube i surrounded by a cylinder, 2, of Transito or the like and closed at its upper end by a dished plate, 4, which carries centrally depending from its bottom a cupped container, 5, in which is housed a booster charge, 7.
  • a firing squib, 9, carried by the top plate, 4, projects into the booster, and is adapted to be connected as by the wire, 10, to electrical firing means, not shown, whereby the device may be fired froml a safe distance.
  • the container is closed on the bottom by a cupped reentrant wall, l2, fitted into the tube, l, and preferably secured thereto by cement, to retain the Thermit burning charge, l5.
  • the gaps between the lower edges of the Thermit unit and the mine case may be sealed as by means of a clay or sand pack to retain the molten iron for a sufficient length of time.
  • the Thermit reaction creates a pool of molten iron on top of the case, having an area of approximately 5G sq. in., which area of the case is heated to the melting point of iron, producing an opening roughly equal in area to the cross-section of the burning charge. It has been found, however, that this type of Thermit unit is best used so as to allow the pool of liquid iron to form, that is, it should not be placed on the side of a mine, nor should it be supported above a mine, or placed on an object of curvature or radius so small as to allow seine of the material to escape. The operation of such a unit further seems to be limited to steel case thicknesses of not greater than .25.
  • FIGURE 5 a modified technique which involves the use of a Crucible unit designed 4to discharge a greater quantity of molten iron, in a smaller stream, against the case to be entered.
  • FIGURE 5 a suitable manner of supporting it in operation is indicated in FIGURE 4.
  • the ven-t of the Crucible should be located from 2 to 4 inches above the surface or case, and somewhat off-center, so that the stream of iro-n will impinge on a sloping surface.
  • a six to ten-pound Thermit charge has been found to be adequate.
  • the refractory crucible, lA is open at its top, the ⁇ bottom ybeing formed with a relatively small discharge opening, Ztl.
  • the Crucible may be enclosed in a sheet metal container as 2A, having a sheet metal Ibottom cap, liZA, adapted to be melted through after retaining the Thermit material and molten iron untill the reaction is well initiated.
  • the firing squib, 9A, and booster charge, 7A are indicated on top of the main charge, and as shown in FIGURE 5, the crucible assembly may be supported upon a simple scaffold generally designated 22. Electric leads, 10A, permitting operation from a safe distance may be connected to suitable electrical firing means (not shown).
  • the charge When the charge is ignited, it first burns a hole in the bomb Ycase and then enters the interior, igniting the explosive content. Explosive materials of the ordinary types used in ordnance burn relatively quietly when so ignited. If the charge contains aluminum or other metallic reducing agents, the reaction may, rather than an ordinary burning, consist of an auto reduction reaction with formation of aluminum oxide and gas as mentioned above in connection with underwater disposal. IIf no reducing agent is present, as in the case of pure TNT, the material may be destroyed by straght burning at the orifice created inthe case. The action is regenerative, that is, a part of the flame serves to heat the charge and the container, in turn maintaining vola-tilization of the explosive and feeding the flame.
  • the cylindrical case, 1B is preferably for-med of insulating material having great resistance to thermal shock and considerable mechanical strength.
  • the best material thus far found for this use is sold under the trade name Transita Such material is also easy to fabricate and machine.
  • Top and bottom closure plates, 4B, 12B, respectively may be bolted in place, as shown, to secure the Thermit char-ge, 15B, which is preferably formed of nonmagnetic hematite.
  • the closure plates project radially beyond the remainder of the casing and are perforated in vertical alignment, to receive supporting rods 22B.
  • Rods 22B are pointed at their lower ends and project below the assembly to suppont the same, being adjustably attached by means of manually yoperable clamping screws 23B.
  • the electrical connection to the squib is provided through the top plate, 4B a pressure resistant connector, 24, being provided at this point having a suitable terminal at its outer end to ⁇ which the lead 10B may be connected as shown.
  • a simple oneway piston valve consisting of a piston element, 27, housed in cylinder, 29, connected to the top of the unit and communicating with the interior thereof via passage, 30.
  • a soft rubber gasket, 32 is arranged between the piston, 27, and the shoulder 31 formed by the counterbored portion of the cylinder, 29, in which the piston is housed, the piston being tightly held against the cylinder by the cotter pin, 33 which is removed before tiring, the piston thereafter being held in place by hydrostatic pressure.
  • piston, 27, and gasket, 32 may be cemented together, Iand against the shoulder, 31, space being left between the piston, 27, and cotter pin, 33, and the lit of the piston being loose enough to permit escape of pressure therearound when it is unseated and the cement seal is broken.
  • the piston may be forced olf its seat by sufficient internal pressure.
  • the piston when the internal pressure rises suiciently, the piston is discharged from the opening and entrance of sea water is prevented during the reaction by the continuous gaseous discharge.
  • the device In operation, the device is simply positioned upon the mine or other device to be entered, and fired from a safe distance.
  • the unit generates a pool of molten iron, as Will be readily apparent, and releases it in a jet against the case upon which the device is positioned.
  • the molten iron melts Iits way into the interior of the case and initiates the above described reaction, which progresses until the explosive charge is destroyed.
  • acoustically operable mines which might be detonated by the ring of the squib and booster of my mechanism, are usualy also equipped with anti-countermining 'devices arranged to prevent detonation if the noise is in the form of a Suiciently loud report, I preferably also re a dctonator or other small quantity of explosive simultaneously, to actuate the anticountermining means.
  • This supplemental, paralyzing charge such as 4tlg FIG. 6, may of course be fired against or close to lthe mine by the same wiring and electrical means, its squib being simply connected in parallel with the squib 9, 9A or 9B.
  • An apparatus for destroying an encased explosive charge comprising a housing, means for supporting said housing adjacent the outer surface or" the casing, said housing having a discharge aperture therein which is substantially smaller in cross section than that of the housing, a fusible closure cap mounted on the housing and over said aperture, a Thermit material contained in said housing, and remote control means for igniting the Thermit whereby the products of the Therrnit reaction penetrate the ⁇ fusible closure cap and ilow from the 4aperture in a concentrated stream to burn through the casing and initiate a slow exothermic combustion of the explosive charge IWithout high order detonation thereof.
  • An apparatus for destroying an encased explosive charge comprising a hermetically sealed housing positioned adjacent the outer sur-face of said casing, said housing having a discharge aperture ⁇ in the bottom thereof, a -fusible closure cap mounted on the housing and over the aperture, a pressure actuated vent mounted on said housing and communicating with the interior thereof, a Thermit material contained within said housing, means to ignite said Thermit material whereby the gaseous products of the Thermit reaction escape from the housing through said pressure actuated vent and the molten products of the Thermit reaction penetrate the fusible closure cap and dlow from the aperture to burn through the casing to initiate a slow exothermic combustion of the explosive charge Vwithout. high order detonation thereof.
  • a hermetically sealed housing means for supporting the housing adjacent the outer surface of the casing, said housing havin-g a discharge aperture therein which is of a substantially smaller cross-sectional area than that of the housing, a fusible closure cap mounted on the housing and over the aperture, a Thermit material contained within said housing, means to ignite said material, a time delay means to permit all of the Therm'it to be reduced to a molten mass, and a pressure actuated vent mounted on the housing and comv municating with the interior thereof vwhereby excessive pressures produced by the rhermit reaction may be released, said molten mass penetrating the Ifusible cap and flowing from the aperture in a concentrated stream to bum through the casing to initiate a slow exothermic combustion of the explosive charge Without high order detonation thereof.
  • the method of destroying an encased explosive charge which comprises igniting an external source of heat, exploding a paralyzing charge adjacent the encased explosive simultaneously With the ignition of said heat source to activate any anticountermining device which may be Y protecting said explosive, directing the heat source against the casing containing the explosive charge to burn an opening therethrough, and heating a portion of the explosive adjacent the opening sufficiently to initiate and cause exothermic combustion of substantially all of said material without high order detonation thereof.
  • the method of destroying an encased explosive charge which comprises positioning a source of heat adjacent the outer surface of the casing, rapidly burning an opening of substantial size through the casing to expose the explosive charge, and applying the source of heat to the exposed explosive to initiate and cause an exothermic combustion of substantially all of said charge Without high order detonation thereof.
  • the method of destroying an encased explosive material which comprises positioning a housing contained a quantity of Thermit above the outer casing containing the explosive, igniting the Therrnit, burning a hole through the outer casing to expose the explosive by directing the molten iron resulting from the Therrnit reaction against the casing, and heating the exposed explosive with the molten iron which has penetrated the casing to initiate and cause relatively slow exothermic combustion of the explosive charge.

Description

Nov. 5, 1963 H. J. PLuMLl-:Y 3,109,369
DISPOSAL oF ENcAsED ExPLosI'vEs Filed May s1, 1944 2 sheets-sheet 2 United States Patent O 3,139,369 DISPSAL F ENCASED 'EXPLGSVES Harold l. Plumley, Z364 Skyland Piana, Washington, DHS. Filed May Si, 1944, Ser. No. 38,l73 7 Claims. (Ci. 102-1) (Granted under Title 35, U5. Code (1952), sec. 266) This invention relates to the disposal of explosive-bearing ordnance by techniques involving either a simple burning of the explosive charge in fair, the necessary oxygen being supplied by the air, and/or by a self-sustaining reductive reaction requiring no air or oxygen supply, and which may accordingly be effected under water.
An important object of the invention is to provide improved means whereby the explosive charges of bombs, mines, depth charges rand other explosive-bearing ordnance may be removed in a quick, simple and eliicient manner, with the least possible risk of high Korder detonation.
Another object is to provide such means which requires, in order to effectuate the removal of the explosive charge, only relatively light, compact and easily portable apparatus, and which, further, involves the use of apparatus which may be operated from a safe distance and which may be set up Without creating such mechanical disturbance or magnetic etect as might initiate an unwanted detonation in event the ordnance should be equipped with anti-magnetic and/ or anti-disturbance devices or the like.
While dangers and diiculties have been encountered in depotentiating such items of ordnance on land, tthe problems are greatly aggravated in dealing with underwater ordnance. In fact lit has usually been considered impossible to render mines and the like safe under water otherwise than by detonating them. Attempts to move or raise a ground mine from the bottom usually result in its firing, since acoustic or magnetic anti-disturbance devices, `or both, are usually present. Hydrostatic switches which tire the mine upon the decrease of water pressure which occurs when it is raised are also very commonly fitted. Although in principle a diver might render safe certain of the more simple ground mine devices under water, `as by removing the detonator, blocking the hydrostatic switch, etc., the `hazard of this work is obvious, and is prohibitive in a practical sense, because of the poor visibility and diflicult working conditions, and the lack of complete access to the mine, which is usually partially buried in the sea bottom. Removal of the fuze or detonator, or both, may also be prevented by the inclusion of anti-withdrawal devices, and the removal of these devices may also be impossible because of their inaccessible positioning, as indicated, particularly if the mine is imbedded in the sea bottom. Booby traps are also used to prevent disturbing these elements without firing the mine. When it is considered in addition that such mines are usually fitted with live acoustic devices arranged to cause the mine to tire in event of any substantial noise in the vicinity, it will be understood that rendering such mines safe, by means entailing .the performance of :any substantial amount of manual work thereon, is virtual-ly impossible.
Since some of the same considerations obtain with respect -to efforts to render harmless bombs, mines, etc., located above ground, it has become increasingly common practice to render them safe by removing the main charge. Above ground this may be done by steaming out the main charge, by the use of solvents, by washing out the charge, or by burning. Any of these procedures are impractical beneath the water.
The present invention also includes among its objects, therefore, the overcoming of the indicated diliiculties, and the entirely safe destruction of explosive-bearing ordnance under tlhe diiiicult conditions outlined.
ice
Another object of this invention is to provide such means involving a construction formed entirely of nonferrous materials, which may be loaded with non-magnetic Therrnit, so that danger of tiring a mine or other explosive device equipped with magnetically responsive elements is eliminated.
Another object is to provide such a mechanism which is capable of withstanding the great thermal shock involved in the rapid development of a thermal gradient of about 4000D F. across the wall thickness of .the unit, and the rapid cooling eifect of the surrounding water.
Another object is to provide such a mechanism having delay means adapted to prevent the release of the Thermit until approximately l5 seconds have elapsed after ignition of the charge, to insure that the Thermit reacts with reasonable completeness before such reaction is stopped by release of the molten iron.
Still another object is to provide electric ignition means, and to protect the electrical lead-in and other means lassociated therewith against the high pressures which may be involved and which may be applied from either or both sides.
Still another object is to prov-ide such a mechanism incorporated in a simple, unitary compact construction which is :absolutely waterproof to depths of at leas-t 200 feet, and which is capable of withstanding the conside-rable internal pressures developed during the reaction period. Still another object is to provide such a unit which is light in weight and which is in stable equilibrium when placed on a cylindrical or -spherical surface underwater, and which is able to maintain itself in position under gravity and without special attaching means, under ordina-ry conditions.
Other objects and advantages will be apparent from the following description taken `in conjunction with the drawings forming a part of the present disclosure.
ln the drawing, in which like reference characters designate similar parts throughout the several views:
FIGURE l is a perspective view of a mine to which is shown attached a preferred means for initiating self-destruction in accordance with the present invention;
FIGURE 2 is a vertical, substantially diametric crosssection of the initiating device, taken substantially on the line 2 2 `of FIGURE l and looking in the direction of the arrow;
FEC-URE 3 is a sectional detail taken substantially on the line 3 3 of FXGURE 2 and looking in the direction of the arrow;
FIGURE 4 is a perspective v-iew of a bomb, together with rigging, and an initiating device supported by the rigging7 such devicve being or" somewhat modified construction;
FIGURE 5 is a vertical substantial-ly dametric sectional view taken substantially on the line 5 5 of FIGURE 4 and looking in the direction of the arrow;
FIGURE 6 is a vertical substantially diametric crosssectional view of a unit constructed in accordance with the present invention and suitable for underwater use, showing the same in position upon a mine case, which is fragmentarily illustrated; and
FIGURE 7 is 'a view partly in top plan and partly in cross-section taken Isubstantially on the line 7 7 of FlGURE 6 and looking in the direction of the arrow.
I have found that it the high explosive charge contains aluminum :or some other reducing agent, a slow, selfdestructive reaction may be initiated under water as well as above ground, by exposing the charge to a temperature of about 2500" F. for a short time, and that furthermore, Ksuch self-destructive reaction will continue and spread throughout the charge, destroying it completely with no danger whatsoever of causing detionation of any part of the charge. The essential feature of this reaction is apparently the progressive reduction of the nitrated organic constituents of the explosive by the metallic aluminum. The solid end product is a porous ash, a typical sample of which has been found to be composed of 94% aluminum oxide and 6% carbon. Ammonia is prominent among the gaseous end products of the reaction. Apparently the necessary and suficient condition of the initiation of this reaction is the presence in the high explosive of between lO and 50% of any finely divided metallic reducing agent such as aluminum, magnesium or zinc. Aluminum is the most commonly used agent, and since the aluminizing of exposives for underwater ordnance results in such a wellestablished enhancement of explosive power, the use of such material will probabiy be continued, or at least the use of some comparable reducing agent which will afford the same possibility of destroying the charge by my improved method.
I have also found that non-violent self-destruction of explosives under water may be made to occur by ano-ther type of reaction which differs from the above described auto reduction in that it takes place in certain explosives which are entirely free of metall-ic reducing agents and the end products of which seem to be entirely gaseous, no ash whatever being left. This reaction is apparently a slow exothermic decomposition started by local heating of the charge, and it progresses automatically due to the heat yield of the reaction. Thus far it has been determined that the condition for the sub-surface auto-decomposition reaction in this manner is the presence in the explosive of either hexanitrodiphenylamine or cyclonite. This reaction also occurs Without violence and with a rate of gaseous discharge which is entirely mode-rate.
In accordance with my preferred method, the case of the explosive-bearing ordnance is penetrated and charge ignition initiated, in a single operation, by allowing a pool or jet of molten iron, obtained from a Thermit reaction, to contact `or irnpinge upon the mine or bomb.
FIGURES 1, 2 and 3 show a suitable T hermit crucible adapted to be used in air, by placing the same upon the case of the item of ordnance to be depotentiated. The Thermit may be fired from a distance by means of a squib which is electrically operable. Preferably n-o magnetic materials are used in the construction of the crucible, and hematite base Thermit is used, since it is non-magnetic, unless it is certain that the mine or other ordnance is so designed that it is not sensitive to magnetic materials, in which event black magnetite base Thermit may be used, since it affords greater burning speed.
In the embodiment of FIGURES 1, 2 and 3, a unitary Thermit burning charge l is housed in a container formed of a cylindrical tube i surrounded by a cylinder, 2, of Transito or the like and closed at its upper end by a dished plate, 4, which carries centrally depending from its bottom a cupped container, 5, in which is housed a booster charge, 7. A firing squib, 9, carried by the top plate, 4, projects into the booster, and is adapted to be connected as by the wire, 10, to electrical firing means, not shown, whereby the device may be fired froml a safe distance. The container is closed on the bottom by a cupped reentrant wall, l2, fitted into the tube, l, and preferably secured thereto by cement, to retain the Thermit burning charge, l5. An asbestos ring, 17, controls the area of the molten iron stream which is irst discharged against the case, and the bottom wall delays for a slight and desirable interval the access of the material to the case of the mine or other ordnance, allowing the Thermit reaction to =be well initiated before the material is released. If the assembly is formed of cylindrical tubular parts, in the manner indicated, it will be apparent that it will be stable when placed upon spherical surfaces within a wide range of radii and that the lower end of the container will make good contact with such surfaces. If the article to be de-armed, however, is of some other configuration, as in the case of the cylindrical mine illustrated, the gaps between the lower edges of the Thermit unit and the mine case may be sealed as by means of a clay or sand pack to retain the molten iron for a sufficient length of time.
when the unit is fired, the Thermit reaction creates a pool of molten iron on top of the case, having an area of approximately 5G sq. in., which area of the case is heated to the melting point of iron, producing an opening roughly equal in area to the cross-section of the burning charge. It has been found, however, that this type of Thermit unit is best used so as to allow the pool of liquid iron to form, that is, it should not be placed on the side of a mine, nor should it be supported above a mine, or placed on an object of curvature or radius so small as to allow seine of the material to escape. The operation of such a unit further seems to be limited to steel case thicknesses of not greater than .25.
In order to perform a similar operation upon mines having thicker cases and/or different shapes, I have provided a modified technique which involves the use of a Crucible unit designed 4to discharge a greater quantity of molten iron, in a smaller stream, against the case to be entered. The construction of such a unit is illustrated in FIGURE 5, and a suitable manner of supporting it in operation is indicated in FIGURE 4. Preferably the ven-t of the Crucible should be located from 2 to 4 inches above the surface or case, and somewhat off-center, so that the stream of iro-n will impinge on a sloping surface. For steel case thicknesses up to and including .375, a six to ten-pound Thermit charge has been found to be adequate. As` shown in FIGURE 5, the refractory crucible, lA, is open at its top, the `bottom ybeing formed with a relatively small discharge opening, Ztl. The Crucible may be enclosed in a sheet metal container as 2A, having a sheet metal Ibottom cap, liZA, adapted to be melted through after retaining the Thermit material and molten iron untill the reaction is well initiated. The firing squib, 9A, and booster charge, 7A, are indicated on top of the main charge, and as shown in FIGURE 5, the crucible assembly may be supported upon a simple scaffold generally designated 22. Electric leads, 10A, permitting operation from a safe distance may be connected to suitable electrical firing means (not shown).
When the charge is ignited, it first burns a hole in the bomb Ycase and then enters the interior, igniting the explosive content. Explosive materials of the ordinary types used in ordnance burn relatively quietly when so ignited. If the charge contains aluminum or other metallic reducing agents, the reaction may, rather than an ordinary burning, consist of an auto reduction reaction with formation of aluminum oxide and gas as mentioned above in connection with underwater disposal. IIf no reducing agent is present, as in the case of pure TNT, the material may be destroyed by straght burning at the orifice created inthe case. The action is regenerative, that is, a part of the flame serves to heat the charge and the container, in turn maintaining vola-tilization of the explosive and feeding the flame. This continues until the bomb or mine is completely empty or until the reaction is stopped by some sort of low order detonation. Such detonations may occur near tbe end of the burning, and usually, when the charge has been reduced tot Stich proportions that danger of any lsubstantial destruction by such detonation is Virtually eliminated.
In the underwater embodiment of FIGURES 6 and 7, the cylindrical case, 1B, is preferably for-med of insulating material having great resistance to thermal shock and considerable mechanical strength. The best material thus far found for this use is sold under the trade name Transita Such material is also easy to fabricate and machine. Top and bottom closure plates, 4B, 12B, respectively, may be bolted in place, as shown, to secure the Thermit char-ge, 15B, which is preferably formed of nonmagnetic hematite. The closure plates project radially beyond the remainder of the casing and are perforated in vertical alignment, to receive supporting rods 22B.
Rods 22B are pointed at their lower ends and project below the assembly to suppont the same, being adjustably attached by means of manually yoperable clamping screws 23B. An annular or refractory frustoco-nic bottom portion 17B, anranged directly above the bottom plate 12B, defines the effective size of the discharge opening 20B. This opening is closed by a thin brass platte 13B which quickly :burns through when the molten iron is discharged, additional delay being interposed by the use of a thin layer of slow-.burning bonded Thermit, 16B. It will be apparent that the thickness and characteristics of this layer may be varied to provide any desired delay.
A booster charge 7B, -housed in a can 5B, is suspended in the Thermit charge by means of a strap 25, an electrically operable firing squib, 9B, being arranged in the can B. The electrical connection to the squib is provided through the top plate, 4B a pressure resistant connector, 24, being provided at this point having a suitable terminal at its outer end to `which the lead 10B may be connected as shown.
The development of unduly high internal pressures within the unit is prevented by the use of a simple oneway piston valve, consisting of a piston element, 27, housed in cylinder, 29, connected to the top of the unit and communicating with the interior thereof via passage, 30. A soft rubber gasket, 32, is arranged between the piston, 27, and the shoulder 31 formed by the counterbored portion of the cylinder, 29, in which the piston is housed, the piston being tightly held against the cylinder by the cotter pin, 33 which is removed before tiring, the piston thereafter being held in place by hydrostatic pressure. Alternatively, the piston, 27, and gasket, 32, may be cemented together, Iand against the shoulder, 31, space being left between the piston, 27, and cotter pin, 33, and the lit of the piston being loose enough to permit escape of pressure therearound when it is unseated and the cement seal is broken. A
The piston may be forced olf its seat by sufficient internal pressure. In the arrangement first described, when the internal pressure rises suiciently, the piston is discharged from the opening and entrance of sea water is prevented during the reaction by the continuous gaseous discharge.
In operation, the device is simply positioned upon the mine or other device to be entered, and fired from a safe distance. The unit generates a pool of molten iron, as Will be readily apparent, and releases it in a jet against the case upon which the device is positioned. The molten iron melts Iits way into the interior of the case and initiates the above described reaction, which progresses until the explosive charge is destroyed.
In View of the fact that acoustically operable mines, which might be detonated by the ring of the squib and booster of my mechanism, are usualy also equipped with anti-countermining 'devices arranged to prevent detonation if the noise is in the form of a Suiciently loud report, I preferably also re a dctonator or other small quantity of explosive simultaneously, to actuate the anticountermining means. This supplemental, paralyzing charge, such as 4tlg FIG. 6, may of course be fired against or close to lthe mine by the same wiring and electrical means, its squib being simply connected in parallel with the squib 9, 9A or 9B.
It will be apparent that when the technique herein described yis use, it is not necessary for personnel to be near the explosive ordnance for more than a very short length of time. Neither is it necessary to disturb the mine or bomb, so that danger of accidental detonation is virtually eliminated.
The invention herein described may be manufactured and used by or for the Government of the United States of America lfor governmental purposes without the payment of any royalties thereon or therefor.
` I claim:
l. An apparatus for destroying an encased explosive charge comprising a housing, means for supporting said housing adjacent the outer surface or" the casing, said housing having a discharge aperture therein which is substantially smaller in cross section than that of the housing, a fusible closure cap mounted on the housing and over said aperture, a Thermit material contained in said housing, and remote control means for igniting the Thermit whereby the products of the Therrnit reaction penetrate the `fusible closure cap and ilow from the 4aperture in a concentrated stream to burn through the casing and initiate a slow exothermic combustion of the explosive charge IWithout high order detonation thereof.
2. An apparatus for destroying an encased explosive charge comprising a hermetically sealed housing positioned adjacent the outer sur-face of said casing, said housing having a discharge aperture `in the bottom thereof, a -fusible closure cap mounted on the housing and over the aperture, a pressure actuated vent mounted on said housing and communicating with the interior thereof, a Thermit material contained within said housing, means to ignite said Thermit material whereby the gaseous products of the Thermit reaction escape from the housing through said pressure actuated vent and the molten products of the Thermit reaction penetrate the fusible closure cap and dlow from the aperture to burn through the casing to initiate a slow exothermic combustion of the explosive charge Vwithout. high order detonation thereof. s
3. In an apparatus vfor destroying an explosive having a surrounding casing, a hermetically sealed housing, means for supporting the housing adjacent the outer surface of the casing, said housing havin-g a discharge aperture therein which is of a substantially smaller cross-sectional area than that of the housing, a fusible closure cap mounted on the housing and over the aperture, a Thermit material contained within said housing, means to ignite said material, a time delay means to permit all of the Therm'it to be reduced to a molten mass, and a pressure actuated vent mounted on the housing and comv municating with the interior thereof vwhereby excessive pressures produced by the rhermit reaction may be released, said molten mass penetrating the Ifusible cap and flowing from the aperture in a concentrated stream to bum through the casing to initiate a slow exothermic combustion of the explosive charge Without high order detonation thereof.
4. The method of destroying an encased explosive charge which comprises bur-ning an opening of substantial size through the casing containing the explosive material, and locally heating a portion of the explosive adjacent the opening sufficiently to initiate and cause exothermic combustion of substantially all of said material without high order detonation thereof.
5. The method of destroying an encased explosive charge which comprises igniting an external source of heat, exploding a paralyzing charge adjacent the encased explosive simultaneously With the ignition of said heat source to activate any anticountermining device which may be Y protecting said explosive, directing the heat source against the casing containing the explosive charge to burn an opening therethrough, and heating a portion of the explosive adjacent the opening sufficiently to initiate and cause exothermic combustion of substantially all of said material without high order detonation thereof.
6. The method of destroying an encased explosive charge which comprises positioning a source of heat adjacent the outer surface of the casing, rapidly burning an opening of substantial size through the casing to expose the explosive charge, and applying the source of heat to the exposed explosive to initiate and cause an exothermic combustion of substantially all of said charge Without high order detonation thereof.
7. The method of destroying an encased explosive material which comprises positioning a housing contained a quantity of Thermit above the outer casing containing the explosive, igniting the Therrnit, burning a hole through the outer casing to expose the explosive by directing the molten iron resulting from the Therrnit reaction against the casing, and heating the exposed explosive with the molten iron which has penetrated the casing to initiate and cause relatively slow exothermic combustion of the explosive charge.
References Cited in the le of this patent UNITED STATES PATENTS 8 Wilson Sept. 26, 1944 Lawrence Nov. 21, 1944 Hopkins July 23, 1946 Piggot et a1 Dec. 20, 1949 FOREIGN PATENTS Great Britain Mar. 23, 1898 Great Britain July 14, 1919 Great Britain Mar. 13, 1924 Great Britain Oct. 12, 1942 OTHER REFERENCES Military Explosives, published in 1919 by Govt Printing Oflce, page 101, copy in Div. 30.

Claims (1)

1. AN APPARATUS FOR DESTROYING AN ENCASED EXPLOSIVE CHARGE COMPRISING A HOUSING, MEANS FOR SUPPORTING SAID HOUSING ADJACENT THE OUTER SURFACE OF THE CASING, SAID HOUSING HAVING A DISCHARGE APERTURE THEREIN WHICH IS SUBSTANTIALLY SMALLER IN CROSS SECTION THAN THAT OF THE HOUSING, A FUSIBLE CLOSURE CAP MOUNTED ON THE HOUSING AND OVER SAID APERTURE, A THERMIT MATERIAL CONTAINED IN SAID
US538173A 1944-05-31 1944-05-31 Disposal of encased explosives Expired - Lifetime US3109369A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US538173A US3109369A (en) 1944-05-31 1944-05-31 Disposal of encased explosives
US353692A US3054349A (en) 1944-05-31 1953-05-07 Disposal of encased explosives

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US538173A US3109369A (en) 1944-05-31 1944-05-31 Disposal of encased explosives
US353692A US3054349A (en) 1944-05-31 1953-05-07 Disposal of encased explosives

Publications (1)

Publication Number Publication Date
US3109369A true US3109369A (en) 1963-11-05

Family

ID=26998055

Family Applications (2)

Application Number Title Priority Date Filing Date
US538173A Expired - Lifetime US3109369A (en) 1944-05-31 1944-05-31 Disposal of encased explosives
US353692A Expired - Lifetime US3054349A (en) 1944-05-31 1953-05-07 Disposal of encased explosives

Family Applications After (1)

Application Number Title Priority Date Filing Date
US353692A Expired - Lifetime US3054349A (en) 1944-05-31 1953-05-07 Disposal of encased explosives

Country Status (1)

Country Link
US (2) US3109369A (en)

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4779511A (en) * 1985-07-09 1988-10-25 The United States Of America As Represented By The Secretary Of The Navy Disposal dearmer for EOD applications
US5353676A (en) * 1993-12-27 1994-10-11 The United States Of America As Represented By The Secretary Of The Army Apparatus and method for remote disassembly of failed high explosive type mine
FR2742539A1 (en) * 1995-12-14 1997-06-20 Giat Ind Sa Multi-purpose explosive charge, e.g. for detonating mines
US5936184A (en) * 1997-11-21 1999-08-10 Tracor Aerospace, Inc. Devices and methods for clearance of mines or ordnance
US6484617B1 (en) 1999-05-10 2002-11-26 Alliant Techsystems Inc. Assembly and process for controlled burning of landmine without detonation
DE10058325B4 (en) * 2000-08-09 2004-04-15 Eads Deutschland Gmbh Clearing device for a detention mine
US20050222484A1 (en) * 1997-11-24 2005-10-06 Science Applications International Corporation Method and apparatus for mine and unexploded ordnance neutralization
US7331268B1 (en) 2004-06-02 2008-02-19 The United States Of America As Represented By The Secretary Of The Navy Explosive neutralization method and device
US20120017750A1 (en) * 2009-03-31 2012-01-26 Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) Blast treatment method and blast treatment device
US20130139715A1 (en) * 2011-06-13 2013-06-06 Eric Bleicken Reactive material breaching device
RU2485437C1 (en) * 2012-02-07 2013-06-20 Федеральное государственное военное образовательное учреждение высшего профессионального образования Военная академия Ракетных войск стратегического назначения имени Петра Великого МО РФ Method of disassembly of munitions
RU2493536C2 (en) * 2011-08-05 2013-09-20 Федеральное Государственное Военное Образовательное Учреждение Высшего Профессионального Образования Военный Учебно-Научный Центр Сухопутных Войск "Общевойсковая Академия Вооруженных Сил Российской Федерации" (Ова Вс Рф) Method to recycle black rifle powder by bullet shot of small arms
DE102009021820B4 (en) * 2009-05-18 2014-01-16 Rheinmetall Waffe Munition Gmbh Apparatus and method for destruction of ammunition or the like
WO2014037905A1 (en) * 2012-09-07 2014-03-13 Kuhn Petrus Gerhardus Deflagration arrangement for neutralising explosives
DE102013004445B3 (en) * 2013-03-15 2014-05-22 Frank Bargmann Method for recovering and defusing bombs lying on seabed, involves dismantling bomb in chamber by high pressure water jet device, after introducing air into space under displacing water
US9175938B2 (en) 2011-06-13 2015-11-03 Darrel Barnette Rotating and oscillating breaching device with reactive material
US9365463B1 (en) 2011-06-13 2016-06-14 Darrel Barnette Rotating and oscillating breaching device with reactive material
US9709370B1 (en) * 2016-05-13 2017-07-18 Captive Technologies, LLC Transporting and disposing of recalled airbag inflators
DE102017108833A1 (en) 2017-04-25 2018-10-25 Rheinmetall Waffe Munition Gmbh neutralizing body
RU2714165C1 (en) * 2018-12-03 2020-02-12 ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ КАЗЕННОЕ ВОЕННОЕ ОБРАЗОВАТЕЛЬНОЕ УЧРЕЖДЕНИЕ ВЫСШЕГО ОБРАЗОВАНИЯ "Военная академия Ракетных войск стратегического назначения имени Петра Великого" МИНИСТЕРСТВА ОБОРОНЫ РОССИЙСКОЙ ФЕДЕРАЦИИ Ammunition reloading method
US11187512B1 (en) * 2019-08-29 2021-11-30 The United States Of America As Represented By The Secretary Of The Navy Apparatus for detonating munitions

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3173364A (en) * 1962-03-24 1965-03-16 Military Training Device Compa Ammuntion safety device
US3724372A (en) * 1963-10-30 1973-04-03 Us Navy Pyrojet cutter for underwater or land use
US4046055A (en) * 1975-07-18 1977-09-06 The United States Of America As Represented By The Secretary Of The Army Apparatus for safely neutralizing explosive devices
US4280409A (en) * 1979-04-09 1981-07-28 The United States Of America As Represented By The Secretary Of The Navy Molten metal-liquid explosive device
FR2558949B1 (en) * 1984-01-31 1987-06-19 Buon Christiane PROPULSED PLATE FOR NEUTRALIZATION OF REMOTE SUSPECT DEVICES
US4727789A (en) * 1986-06-24 1988-03-01 T & E International, Inc. Vented suppressive shielding
US4942820A (en) * 1988-11-14 1990-07-24 Sawruk Stephen D Fragmentation device
US6553911B1 (en) 1997-04-30 2003-04-29 Erico International Corporation Exothermic reactions and methods
WO2003064095A2 (en) 2002-01-25 2003-08-07 Erico International Corporation Welding apparatus and method
US8495959B2 (en) * 2006-05-15 2013-07-30 Exquadrum, Inc. Kinetic fireball incendiary munition

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB189807100A (en) * 1898-03-23 1898-04-23 Harris Priuli Hurst Improvements in Explosive Shells, and in Fuses or Fuse Fittings for Detonating the Explosive.
US745981A (en) * 1903-02-24 1903-12-01 Charles V Wheeler Delayed-action fuse for projectiles.
GB129759A (en) * 1918-06-13 1919-07-14 Frederick Howard Livens Improvements relating to Bombs, Shells, and the like, more particularly of the Unrifled Class used for Emitting Lethal Vapours.
US1378269A (en) * 1920-01-27 1921-05-17 California Cap Company Electric blasting-cap
GB212357A (en) * 1923-01-15 1924-03-13 Francis Norman Pickett Improvements in and relating to the freeing of the metal casings of shell or the like ammunition from the explosive fillings thereof
US1562137A (en) * 1925-03-18 1925-11-17 Barnes Howard Turner Method of loosening ice accumulations
US1797509A (en) * 1929-03-18 1931-03-24 Du Pont Electric blasting cap and ignition material for the same
GB548450A (en) * 1940-04-10 1942-10-12 Henry Molyneux Lyman Towed means for the harmless destruction of magnetic mines by effecting the detonation thereof
US2358899A (en) * 1941-04-09 1944-09-26 John H Wilson Projectile
US2363254A (en) * 1940-03-23 1944-11-21 Hercules Powder Co Ltd Blasting cap
US2404441A (en) * 1942-02-07 1946-07-23 Raymonde Briggs Hopkins Method of rendering bombs inactive
US2491516A (en) * 1944-01-12 1949-12-20 Charles S Piggot Method and means to safely deactivate explosive bearing ordnance

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1299869A (en) * 1918-06-14 1919-04-08 Joseph A Steinmetz Gun-destroying means.
US2391242A (en) * 1941-02-11 1945-12-18 Clarence B Hurrey Thermit bomb
US2417592A (en) * 1943-08-28 1947-03-18 Aerial Products Inc Smoke generator

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB189807100A (en) * 1898-03-23 1898-04-23 Harris Priuli Hurst Improvements in Explosive Shells, and in Fuses or Fuse Fittings for Detonating the Explosive.
US745981A (en) * 1903-02-24 1903-12-01 Charles V Wheeler Delayed-action fuse for projectiles.
GB129759A (en) * 1918-06-13 1919-07-14 Frederick Howard Livens Improvements relating to Bombs, Shells, and the like, more particularly of the Unrifled Class used for Emitting Lethal Vapours.
US1378269A (en) * 1920-01-27 1921-05-17 California Cap Company Electric blasting-cap
GB212357A (en) * 1923-01-15 1924-03-13 Francis Norman Pickett Improvements in and relating to the freeing of the metal casings of shell or the like ammunition from the explosive fillings thereof
US1562137A (en) * 1925-03-18 1925-11-17 Barnes Howard Turner Method of loosening ice accumulations
US1797509A (en) * 1929-03-18 1931-03-24 Du Pont Electric blasting cap and ignition material for the same
US2363254A (en) * 1940-03-23 1944-11-21 Hercules Powder Co Ltd Blasting cap
GB548450A (en) * 1940-04-10 1942-10-12 Henry Molyneux Lyman Towed means for the harmless destruction of magnetic mines by effecting the detonation thereof
US2358899A (en) * 1941-04-09 1944-09-26 John H Wilson Projectile
US2404441A (en) * 1942-02-07 1946-07-23 Raymonde Briggs Hopkins Method of rendering bombs inactive
US2491516A (en) * 1944-01-12 1949-12-20 Charles S Piggot Method and means to safely deactivate explosive bearing ordnance

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4779511A (en) * 1985-07-09 1988-10-25 The United States Of America As Represented By The Secretary Of The Navy Disposal dearmer for EOD applications
US5353676A (en) * 1993-12-27 1994-10-11 The United States Of America As Represented By The Secretary Of The Army Apparatus and method for remote disassembly of failed high explosive type mine
FR2742539A1 (en) * 1995-12-14 1997-06-20 Giat Ind Sa Multi-purpose explosive charge, e.g. for detonating mines
US5936184A (en) * 1997-11-21 1999-08-10 Tracor Aerospace, Inc. Devices and methods for clearance of mines or ordnance
US20050222484A1 (en) * 1997-11-24 2005-10-06 Science Applications International Corporation Method and apparatus for mine and unexploded ordnance neutralization
US6979758B2 (en) * 1997-11-24 2005-12-27 Science Applications International Corporation Method and apparatus for mine and unexploded ordnance neutralization
US7501551B2 (en) * 1997-11-24 2009-03-10 Science Applications International Corporation Method and apparatus for mine and unexploded ordnance neutralization
US6484617B1 (en) 1999-05-10 2002-11-26 Alliant Techsystems Inc. Assembly and process for controlled burning of landmine without detonation
DE10058325B4 (en) * 2000-08-09 2004-04-15 Eads Deutschland Gmbh Clearing device for a detention mine
US7331268B1 (en) 2004-06-02 2008-02-19 The United States Of America As Represented By The Secretary Of The Navy Explosive neutralization method and device
US8516937B2 (en) * 2009-03-31 2013-08-27 Kobe Steel, Ltd. Blast treatment method and blast treatment device
US20120017750A1 (en) * 2009-03-31 2012-01-26 Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) Blast treatment method and blast treatment device
DE102009021820B4 (en) * 2009-05-18 2014-01-16 Rheinmetall Waffe Munition Gmbh Apparatus and method for destruction of ammunition or the like
US8789468B2 (en) * 2011-06-13 2014-07-29 Eric Bleicken Reactive material breaching device
US9365463B1 (en) 2011-06-13 2016-06-14 Darrel Barnette Rotating and oscillating breaching device with reactive material
US20130139715A1 (en) * 2011-06-13 2013-06-06 Eric Bleicken Reactive material breaching device
US9175938B2 (en) 2011-06-13 2015-11-03 Darrel Barnette Rotating and oscillating breaching device with reactive material
RU2493536C2 (en) * 2011-08-05 2013-09-20 Федеральное Государственное Военное Образовательное Учреждение Высшего Профессионального Образования Военный Учебно-Научный Центр Сухопутных Войск "Общевойсковая Академия Вооруженных Сил Российской Федерации" (Ова Вс Рф) Method to recycle black rifle powder by bullet shot of small arms
RU2485437C1 (en) * 2012-02-07 2013-06-20 Федеральное государственное военное образовательное учреждение высшего профессионального образования Военная академия Ракетных войск стратегического назначения имени Петра Великого МО РФ Method of disassembly of munitions
WO2014037905A1 (en) * 2012-09-07 2014-03-13 Kuhn Petrus Gerhardus Deflagration arrangement for neutralising explosives
DE102013004445B3 (en) * 2013-03-15 2014-05-22 Frank Bargmann Method for recovering and defusing bombs lying on seabed, involves dismantling bomb in chamber by high pressure water jet device, after introducing air into space under displacing water
US9709370B1 (en) * 2016-05-13 2017-07-18 Captive Technologies, LLC Transporting and disposing of recalled airbag inflators
US10072917B2 (en) * 2016-05-13 2018-09-11 Captive Technologies, LLC Barrel containers for transporting and disposing of recalled airbag inflators
US10072918B2 (en) 2016-05-13 2018-09-11 Captive Technologies, LLC Layered mesh containers for transporting and disposing of recalled airbag inflators
DE102017108833A1 (en) 2017-04-25 2018-10-25 Rheinmetall Waffe Munition Gmbh neutralizing body
RU2714165C1 (en) * 2018-12-03 2020-02-12 ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ КАЗЕННОЕ ВОЕННОЕ ОБРАЗОВАТЕЛЬНОЕ УЧРЕЖДЕНИЕ ВЫСШЕГО ОБРАЗОВАНИЯ "Военная академия Ракетных войск стратегического назначения имени Петра Великого" МИНИСТЕРСТВА ОБОРОНЫ РОССИЙСКОЙ ФЕДЕРАЦИИ Ammunition reloading method
US11187512B1 (en) * 2019-08-29 2021-11-30 The United States Of America As Represented By The Secretary Of The Navy Apparatus for detonating munitions

Also Published As

Publication number Publication date
US3054349A (en) 1962-09-18

Similar Documents

Publication Publication Date Title
US3109369A (en) Disposal of encased explosives
US4372213A (en) Molten metal-liquid explosive method
US3117518A (en) Apparatus for cutting encased explosives
US2478958A (en) Pressure release
US3173364A (en) Ammuntion safety device
US4132171A (en) Apparatus for detonating an explosive charge
IL131023A (en) Missile warhead design
EP0601880A2 (en) Perforating gun detonator package incorporating exploding foil
US6253680B1 (en) Diversionary device
US3759216A (en) Smoke flare signalling and marking device
US2925775A (en) Well casing perforator
US2949853A (en) Drill mine
EP0600039A1 (en) Insensitive propellant ignitor
US4962708A (en) Electric/non-electric initiation system
US3291050A (en) Apparatus and method for the demolition of objects
US4030418A (en) Gravity deployed mine with combined upper clearing charge firing and delayed main charge initiation
US5129305A (en) Penetrating assault weapons
US4040354A (en) Gravity-deployed double-ended anti-tank mine
US3995549A (en) Rocket/missile motor explosive insert detonator
US4058060A (en) Gravity-deployed munition with a mechanical gravity-controlled switch
US3216354A (en) Land mine
US2812148A (en) Delayed opening parachute pack
US2712790A (en) Sympathetic or concussion firing device
US2945440A (en) Discriminating fuze
US2960915A (en) Scatter charge