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US20070113939A1 - High energy blast explosives for confined spaces - Google Patents

High energy blast explosives for confined spaces Download PDF

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US20070113939A1
US20070113939A1 US11/482,302 US48230206A US2007113939A1 US 20070113939 A1 US20070113939 A1 US 20070113939A1 US 48230206 A US48230206 A US 48230206A US 2007113939 A1 US2007113939 A1 US 2007113939A1
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nano
sized
metal composite
metal
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May Chan
Alan Turner
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    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B45/00Compositions or products which are defined by structure or arrangement of component of product
    • C06B45/12Compositions or products which are defined by structure or arrangement of component of product having contiguous layers or zones
    • C06B45/14Compositions or products which are defined by structure or arrangement of component of product having contiguous layers or zones a layer or zone containing an inorganic explosive or an inorganic explosive or an inorganic thermic component
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B25/00Compositions containing a nitrated organic compound
    • C06B25/34Compositions containing a nitrated organic compound the compound being a nitrated acyclic, alicyclic or heterocyclic amine
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B33/00Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide

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  • the invention disclosed herein relates to explosive formulations with improved combustion efficiency. More particularly, the explosive formulations of the invention are capable of maintaining a relatively high blast pressure in an oxygen poor environment, such as a tunnel or other confined spaces.
  • Aluminum has been used as the metal of choice, due to high heat of combustion, cost and availability. Billets of SFAE made with Al, provide savings in volume with increased fuel mass for blast performance. However, combustion efficiency has been an issue, especially in the event that the fuel content (35-60 wt %) is high with respect to the total weight of explosive composition. Poor combustion efficiency is often observed in many of the thermobaric warhead tests, which causes the severe ineffectiveness of the weapon. This is due to the high ignition temperature, 2200 K, typically required for proper combustion of AL. During the burning of Al, heat is produced and aluminum oxide is formed. However, the burning of all the metal to completion requires maintaining the hot environment. This environment can be best maintained if it is supported chemically by the combustion of other oxidizer species (i.e.
  • IPN isopropyl nitrate
  • AP has an ignition temperature of 250 C and IPN has a low flash point of 22 C.
  • the combustion of these additives produce the hot gases to support the burning of metal, thus 100% combustion efficiency can be obtained.
  • Metal composites, metal and oxidizer combined granules, produced from coating of particles with a binder, can be made easily with techniques well known in the art.
  • Another combined approach to further improve the metal combustion efficiency is to use a more reactive metal as part of or as the entire metal fuel component.
  • New reactive metal materials such as nano-sized aluminum to increase the reactivity, titanium and boron alloy to increase the thermal output, and magnesium/aluminum alloy to lower the ignition temperature are among the most promising approaches to increase the metal combustion efficiency.
  • More powerful explosives such as CL-20 that are capable of raising the detonation pressure and temperature are also extremely beneficial.
  • the present invention relates to a metal composite that combines a binder, a reactive metal and an oxidizer.
  • a plasticizer and a catalyst are also included.
  • the binder includes polymers capable of coating the reactive metal and oxidizer powder. Two embodiments include methods to produce the compositions of the present invention:
  • An embodiment of the present invention discloses a metal composite comprising about 60 to about 96 weight % of at least one reactive metal, about 4 to about 10 weight % of at least one binder and about 0 to about 36 weight % of an oxidizer.
  • the reactive metal includes, but not limited to at least one of nano-sized metal particles, metastable mechanical alloy and any combination thereof. More specifically, the reactive metal includes, but not limited to at least one of nano-sized aluminum, nano-sized boron and nano-sized titanium, nano-sized magnesium, and nano-sized Al—Mg, Al—Mg—H, B—Mg, Al—B and Ti—B mixtures.
  • the binder includes, but not limited to at least one of copolymer of vinylidine fluoride hexafluoropropylene, nitrocellulose, GAP and Zeon.
  • Embodiments of the present invention relating to castable compositions disclose an explosive having an annular construction.
  • the explosive includes a cylindrical shell of solid fuel air explosive surrounding a cylindrically shaped high explosive.
  • the solid fuel air explosive includes at least one of reactive metal and metal composite.
  • the metal composite including about 60 to about 80 weight % of at least one reactive metal, about 4 to about 8 weight % of at least one binder and about 0 to about 36 weight % of an oxidizer.
  • the reactive metal includes, but is not limited to at least one of nano-sized metal particles, metastable mechanical alloy and any combination thereof.
  • the reactive metal includes at least one of nano-sized aluminum, nano-sized boron and nano-sized titanium, nano-sized magnesium, and nano-sized Al—Mg, Al—Mg—H, B—Mg, Al—B and Ti—B mixtures, H-2 (2 ⁇ m spherical aluminum) and H-5 (5 ⁇ m spherical aluminum).
  • the oxidizer includes, but is not limited to at least one of ammonium perchlorate, ammonium dinitramide and ammonium nitrate.
  • the present invention is to provide an explosive with enhanced combustion efficiently capable of sustaining a high pressure over a period of time in a confined environment with a limited oxygen supply.
  • the present invention is to provide an explosive capable of maintaining a relatively high pressure (30-60 psi) for up to 50 msec in an environment characterized with high rate of thermal quenching (cold air), this environment has a profound adverse effect for metal combustion, which is the main cause for combustion efficiency.
  • blast effectiveness is increased by a factor of two over more conventional explosive devices and
  • embodiments the present invention is to provide an explosive with increased reactivity, increased thermal output and lower ignition temperatures.
  • Embodiments the present invention are also to provide thermobaric explosive formulations with reactive metals and metal composites which have a 100% higher blast energy than compositions such as Tritonal and PBX N109.
  • FIG. 1 is a sectional view of a typical explosive having an annular construction
  • FIG. 2 is a plot illustrating the blast effectiveness of an explosive which includes a reactive metal of nano-meter sized metal particles.
  • the invention disclosed herein relates to an explosive capable of enhanced combustion efficiently capable of sustaining a high pressure over a period of time in a confined environment, such as an air tight room or a cave, where oxygen may be in limited supply.
  • the reactive metal used in an embodiment of the present invention includes nano-sized metal particles, metastable mechanical alloys and any combination thereof.
  • the metal fuel in these explosive formulations of the present invention incorporates nano-sized aluminum, including, for example, Alex®, boron, manganese and titanium, those having a size of about 20-500 nm.
  • the metastable mechanical alloys include nano-sized Al—Mg, Al—Mg—H, B—Mg, Al—B,Ti—B, mixtures and H-2 and H-5 made from high energy milling.
  • the metastable mechanical alloys include nano-crystalline metastable phases with particle sizes of about 1-50 ⁇ m.
  • the reactive metal used also includes Ti, B or Mg. In another embodiment of the present invention, the reactive metal includes about 60-80 weight % of the total metal composite, or at about 74 weight %.
  • thermobaric explosive formulations of the present invention incorporate high energy explosive material including, but not limited to hexa-nitro-hexa-aza-isowurtzitane (CL-20), cyclotrimethylenetrinitramine (RDX) and cyclotetramethylene tetranitramine (HMX).
  • the powerful oxidizers including ammonium perchlorate (AP), ammonium dinitramide (ADN), ammonium nitrate (AN) and barium nitrate are selected to be used in the metal composite or castable PBX's.
  • Another embodiment of the present invention uses ammonium perchlorate (AP) particles, or about 11-100 ⁇ m in size.
  • the oxidizer includes about 12-36 weight % of the total metal composites, or at about 20 weight %.
  • the binder includes polymers capable of coating the reactive metal and high explosive powder.
  • the binder includes, but is not limited to at least one of copolymer of vinylidine fluoride hexafluoropropylene, including Viton®, nitrocellulose, glycidyl azide polymer (GAP) or an acrylic acid ester polymer, including Zeon®.
  • the binder includes about 4-6 weight % of the total metal composites, or at about 4 weight % for the total metal composite.
  • the binders used for castable PBX's include, for example, hydroxy-terminated polybutadienes (HTPB), hydroxy-terminated polycaprolactone (PCP), hydroxy-terminated polyesters, hydroxy-terminated polyethers (HTPE), Glycidyl azide polymer (GAP), trifluoroethyl-terminated poly (1-cyano-1-difluoramino)-polyethylene glycol (PCDE) and any combination thereof. Typically, 5 to 7 weight % is used for castable PBX embodiment.
  • HTPB hydroxy-terminated polybutadienes
  • PCP hydroxy-terminated polycaprolactone
  • HTPE hydroxy-terminated polyesters
  • HTPE hydroxy-terminated polyethers
  • GAP Glycidyl azide polymer
  • PCDE trifluoroethyl-terminated poly (1-cyano-1-difluoramino)-polyethylene glycol
  • a plasticizer and a bum rate catalyst is added.
  • the plasticizer includes bis-(2,2-ro-2-fluoroethyl) formal (FEFO).
  • FEFO bis-(2,2-ro-2-fluoroethyl) formal
  • other plasticizers utilized include energetic plasticizers selected from those compounds, which are liquids and contain energetic moieties or groups in their chemical structures. These moieties include, but not limited to nitro or nitrate ester groups, azido groups, or nitramino groups.
  • Suitable plasticizers include TEGDN (triethyleneglycol dinitrate), or Butyl NENA (n-butyl-2-nitratoethyl-nitramine).
  • plasticizers include DEGDN (diethyleneglycol dinitrate), TMETN (trimethylolethane trinitrate), and BTTN (butanetriol trinitrate). These plasticizers are used independently or in combination.
  • Other fluoramino groups including bis-(2,2-ro-2-fluoroethyl) formal (FEFO) and bis-[2,2-bis(difluoramino)-5,5-dinitro-5-fluoropentoxy] methane (SYFO) could also incorporated into the formulations.
  • the plasticizer include about 4 weight % of the formulations.
  • Iron oxide (Fe 2 O 3 ), nano-sized is a suitable burn rate catalyst and is optional to exotic burn rate catalysts including superfine iron oxide, chromic oxide, catocene, or carboranes. In other embodiments aluminum oxide is also used. In embodiments of the present invention, the burn rate catalyst comprises about 1 weight % of the total metal composites. Tables I and II disclose a number of the formulations of the present invention.
  • Binder ticizer Catalyst 80% H-5 14% AP, 11 ⁇ m 6% Viton ® None None 60% H-5, 20% 14% AP, 11 ⁇ m 6% Viton ® None None Al/Mg alloy, 28 ⁇ m 80% H-5 12% AP, 11 ⁇ m 6% Viton ® None 1% Fe 2O 3 , nano-sized 74% H-5 20% AP, 11 ⁇ m 6% Viton ® None 1% Fe 2O 3 , nano-sized 37% Ti, 44 ⁇ m 21% AP, 11 ⁇ m 6% None None 37% B, 0.6-7 Nitrocellulose ⁇ m 74% Ti—B, 21% AP, 11 ⁇ m 6% None None None 20 ⁇ m Nitrocellulose 74% Mg—B, 21% AP, 11 ⁇ m 6% None None 20 ⁇ m Nitrocellulose 50% H-5 24% 20% AP, 11 ⁇ m 5% None 1% Fe 2 O
  • novel thermobaric explosives of the present invention are spherical particles of composite material containing high explosive, oxidizer, reactive metal and binder. Plasticizer and burn rate catalyst are added to manipulate performance.
  • a method of making the novel thermobaric explosives described herein is disclosed in U.S. Pat. No. 5,750,921 issued to Chan et al. on May 12, 1998, hereby incorporated herein by reference.
  • a solid fuel-air explosive annular construction is used as shown in FIG. 1 .
  • a cylindrical shell of solid fuel air explosive (SFAE) 22 surrounds the high explosive 21 .
  • the shapes of the high explosive charge are include, but not limited to spherically or cylindrically symmetric, to provide a uniform dispersion pattern.
  • Solid metal casings 23 are typically pressed from reactive metal powder or metal composite (listed in Table 1) as SFAE. These solid metal casings are typically machined from stock into billets, but are also manufactured by other methods including casting or forging. The SFAE is then pressed into solid billets with a density (preferred to be 80-90% TMD) applicable to the particular use.
  • PBX N112 consists of 89% HMX (high explosive) and 11% LMA (lauryl methacrylate).
  • the PBX N112/reactive metal weight ratio includes the range of about 0.66 to about 1.45, or the ratio of about 1.
  • Embodiments of the compositions of the present invention are formed into a unicharge.
  • the unicharge construct uses spherical aluminum as the reactive metal.
  • Table II discloses ranges of ingredients for the formulations of the unicharge embodiment.
  • a plasticizer and/or a burn rate catalyst are added to the formulations to tailor the formulations to particular needs.
  • specific binders are listed, any of the binders previously noted are also used in the formulations.
  • any of the oxidizers previously noted are also substituted for AP and any of the high explosives previously noted are substituted for HMX.
  • FIG. 2 there is shown a plot illustrating the blast effectiveness of an explosive which includes a reactive metal of nano-meter sized metal particles.
  • the metal particles used in the explosive have sizes of twenty nano-meters and two hundred nano-meters.
  • the plot represented by the reference numeral 25 is virtually identical for the twenty nano-meter and two hundred nano-meter metal particles. After about 5-10 msec., the plots vary substantially.
  • the plot for the twenty nano-meter metal particles represents a blast effectiveness which is two times that of the two hundred nano-meter metal particles (represented by the reference numeral 26 ). As shown in FIG.
  • the time required for a complete release of energy can be reduced by substantially more than 50 msec and can be as much as 100 msec. Further, by using twenty nano-meter sized metal particles in the explosive device, the time required for total energy release is reduced to approximately 20 msec. which is genrally the maximum time during which total energy release by the explosive device should occur.

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Abstract

The invention disclosed herein relates to an explosive capable of enhanced combustion efficiently capable of sustaining a high pressure over a period of time in a confined environment, such as an air tight room or a cave, where oxygen may be in limited supply. An embodiment of the present invention is a metal composite that combines a binder, a nano-sized reactive metal and an oxidizer. The nano-sized reactive metal has an average particle size of approximetaly 20 nano-meters

Description

    CROSS-REFERENCE TO RELATED APPLICATIONS
  • This application is a continuation-in-part of U. S. patent application Ser. No. 10/779,545, filed Feb. 11, 2004, now U.S. Pat. No. 6,955,732, and U.S. patent application Ser. No. 10/779,548, filed Feb. 11, 2004, which is a divisional of U.S. patent application Ser. No. 10/326,958 filed on Dec. 23, 2002, now U.S. Pat. No. 6,969,434.
  • STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT
  • The invention described herein may be manufactured and used by or for the government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
  • FIELD OF THE INVENTION
  • The invention disclosed herein relates to explosive formulations with improved combustion efficiency. More particularly, the explosive formulations of the invention are capable of maintaining a relatively high blast pressure in an oxygen poor environment, such as a tunnel or other confined spaces.
  • BACKGROUND OF THE INVENTION
  • There is a long history of studying blast explosives, reactive metals and associated metal combustion technologies. The success of the development of Solid Fuel-Air-Explosive (SFAE) has been demonstrated providing 30-40% increased internal blast over a conventional explosive. SFAE is a singular event with combined mixing and initiation of the reaction. In confined spaces, transition to full detonation is not required for enhanced blast, if the solid fuel is ignited early in the dispersion process. A series of reflective shock waves generated by the detonation mixes the hot detonation gases with metal particles and compresses the metal particles at the same time. These actions provide the chemical kinetic support to maintain a hot environment, causing more metal to ignite and burn. This late time metal combustion process produces a significant pressure rise over a longer time duration (10-50 msec). This is a phase generally referred to as after burning or late-time impulse which can occur outside of where the detonation occurred, resulting in more widespread damage.
  • Aluminum has been used as the metal of choice, due to high heat of combustion, cost and availability. Billets of SFAE made with Al, provide savings in volume with increased fuel mass for blast performance. However, combustion efficiency has been an issue, especially in the event that the fuel content (35-60 wt %) is high with respect to the total weight of explosive composition. Poor combustion efficiency is often observed in many of the thermobaric warhead tests, which causes the severe ineffectiveness of the weapon. This is due to the high ignition temperature, 2200 K, typically required for proper combustion of AL. During the burning of Al, heat is produced and aluminum oxide is formed. However, the burning of all the metal to completion requires maintaining the hot environment. This environment can be best maintained if it is supported chemically by the combustion of other oxidizer species (i.e. AP or nitrate ester liquid, IPN (isopropyl nitrate)) that are much easier to ignite (AP has an ignition temperature of 250 C and IPN has a low flash point of 22 C). The combustion of these additives produce the hot gases to support the burning of metal, thus 100% combustion efficiency can be obtained. Metal composites, metal and oxidizer combined granules, produced from coating of particles with a binder, can be made easily with techniques well known in the art.
  • Another combined approach to further improve the metal combustion efficiency is to use a more reactive metal as part of or as the entire metal fuel component. New reactive metal materials such as nano-sized aluminum to increase the reactivity, titanium and boron alloy to increase the thermal output, and magnesium/aluminum alloy to lower the ignition temperature are among the most promising approaches to increase the metal combustion efficiency. More powerful explosives such as CL-20 that are capable of raising the detonation pressure and temperature are also extremely beneficial.
  • There exists a need in the art for new explosive formulations with new reactive metal and metal composites to have 50-100% higher blast energy than those by the baseline composition such as Tritonal or PBX N109. Further, the new formulations coupled with new warhead designs will have the potential to form one of the most powerful thermobaric warheads, when compared to the weapon systems that currently exist.
  • SUMMARY OF THE INVENTION
  • The present invention relates to a metal composite that combines a binder, a reactive metal and an oxidizer. In an embodiment of the present invention, a plasticizer and a catalyst are also included. In yet another embodiment of the present invention, the binder includes polymers capable of coating the reactive metal and oxidizer powder. Two embodiments include methods to produce the compositions of the present invention:
    • (1) The coated powder forms the fuel charge through pressing, combining this fuel charge with a high explosive charge (HMX, RDX or CL-20 based PBX's) in an annular design to make up the fill for the warhead.
    • (2) Using metal or metal/oxidizer powders in a mixing, casting and curing process to combine with high explosive to form castable PBX's. The reactive metal contains ingredients that are intrinsically reactive with the reaction products of high explosive and oxidizer with or without the presence of high concentration of oxygen.
  • An embodiment of the present invention discloses a metal composite comprising about 60 to about 96 weight % of at least one reactive metal, about 4 to about 10 weight % of at least one binder and about 0 to about 36 weight % of an oxidizer. The reactive metal includes, but not limited to at least one of nano-sized metal particles, metastable mechanical alloy and any combination thereof. More specifically, the reactive metal includes, but not limited to at least one of nano-sized aluminum, nano-sized boron and nano-sized titanium, nano-sized magnesium, and nano-sized Al—Mg, Al—Mg—H, B—Mg, Al—B and Ti—B mixtures. The binder includes, but not limited to at least one of copolymer of vinylidine fluoride hexafluoropropylene, nitrocellulose, GAP and Zeon.
  • Embodiments of the present invention relating to castable compositions disclose an explosive having an annular construction. The explosive includes a cylindrical shell of solid fuel air explosive surrounding a cylindrically shaped high explosive. In other embodiments the solid fuel air explosive includes at least one of reactive metal and metal composite. The metal composite including about 60 to about 80 weight % of at least one reactive metal, about 4 to about 8 weight % of at least one binder and about 0 to about 36 weight % of an oxidizer. The reactive metal includes, but is not limited to at least one of nano-sized metal particles, metastable mechanical alloy and any combination thereof. More specifically, the reactive metal includes at least one of nano-sized aluminum, nano-sized boron and nano-sized titanium, nano-sized magnesium, and nano-sized Al—Mg, Al—Mg—H, B—Mg, Al—B and Ti—B mixtures, H-2 (2 μm spherical aluminum) and H-5 (5 μm spherical aluminum). The oxidizer includes, but is not limited to at least one of ammonium perchlorate, ammonium dinitramide and ammonium nitrate.
  • The present invention is to provide an explosive with enhanced combustion efficiently capable of sustaining a high pressure over a period of time in a confined environment with a limited oxygen supply.
  • The present invention is to provide an explosive capable of maintaining a relatively high pressure (30-60 psi) for up to 50 msec in an environment characterized with high rate of thermal quenching (cold air), this environment has a profound adverse effect for metal combustion, which is the main cause for combustion efficiency.
  • Further, when very small metal particles in the order of twenty nano-meters are utilized as the reactive metal in an explosive device made in accordance with the present invention blast effectiveness is increased by a factor of two over more conventional explosive devices and
  • Additionally, embodiments the present invention is to provide an explosive with increased reactivity, increased thermal output and lower ignition temperatures.
  • Embodiments the present invention are also to provide thermobaric explosive formulations with reactive metals and metal composites which have a 100% higher blast energy than compositions such as Tritonal and PBX N109.
  • It is to be understood that the foregoing general description and the following detailed description are exemplary and explanatory only and are not to be viewed as being restrictive of the present invention, as claimed. These and other objects, features and advantages of the present invention will become apparent after a review of the following detailed description of the disclosed embodiments and the appended claims.
  • BRIEF DESCRIPTION OF THE DRAWING
  • FIG. 1 is a sectional view of a typical explosive having an annular construction; and
  • FIG. 2 is a plot illustrating the blast effectiveness of an explosive which includes a reactive metal of nano-meter sized metal particles.
  • DETAILED DESCRIPTION OF THE INVENTION
  • The invention disclosed herein relates to an explosive capable of enhanced combustion efficiently capable of sustaining a high pressure over a period of time in a confined environment, such as an air tight room or a cave, where oxygen may be in limited supply.
  • The reactive metal used in an embodiment of the present invention includes nano-sized metal particles, metastable mechanical alloys and any combination thereof. The metal fuel in these explosive formulations of the present invention incorporates nano-sized aluminum, including, for example, Alex®, boron, manganese and titanium, those having a size of about 20-500 nm. The metastable mechanical alloys include nano-sized Al—Mg, Al—Mg—H, B—Mg, Al—B,Ti—B, mixtures and H-2 and H-5 made from high energy milling. The metastable mechanical alloys include nano-crystalline metastable phases with particle sizes of about 1-50 μm. The reactive metal used also includes Ti, B or Mg. In another embodiment of the present invention, the reactive metal includes about 60-80 weight % of the total metal composite, or at about 74 weight %.
  • The thermobaric explosive formulations of the present invention incorporate high energy explosive material including, but not limited to hexa-nitro-hexa-aza-isowurtzitane (CL-20), cyclotrimethylenetrinitramine (RDX) and cyclotetramethylene tetranitramine (HMX). The powerful oxidizers, including ammonium perchlorate (AP), ammonium dinitramide (ADN), ammonium nitrate (AN) and barium nitrate are selected to be used in the metal composite or castable PBX's. Another embodiment of the present invention uses ammonium perchlorate (AP) particles, or about 11-100 μm in size. The oxidizer includes about 12-36 weight % of the total metal composites, or at about 20 weight %.
  • The binder includes polymers capable of coating the reactive metal and high explosive powder. The binder includes, but is not limited to at least one of copolymer of vinylidine fluoride hexafluoropropylene, including Viton®, nitrocellulose, glycidyl azide polymer (GAP) or an acrylic acid ester polymer, including Zeon®. In another embodiment of the present invention, the binder includes about 4-6 weight % of the total metal composites, or at about 4 weight % for the total metal composite. The binders used for castable PBX's include, for example, hydroxy-terminated polybutadienes (HTPB), hydroxy-terminated polycaprolactone (PCP), hydroxy-terminated polyesters, hydroxy-terminated polyethers (HTPE), Glycidyl azide polymer (GAP), trifluoroethyl-terminated poly (1-cyano-1-difluoramino)-polyethylene glycol (PCDE) and any combination thereof. Typically, 5 to 7 weight % is used for castable PBX embodiment.
  • In other embodiments, a plasticizer and a bum rate catalyst is added. The plasticizer includes bis-(2,2-ro-2-fluoroethyl) formal (FEFO). However, other plasticizers utilized, include energetic plasticizers selected from those compounds, which are liquids and contain energetic moieties or groups in their chemical structures. These moieties include, but not limited to nitro or nitrate ester groups, azido groups, or nitramino groups. Suitable plasticizers include TEGDN (triethyleneglycol dinitrate), or Butyl NENA (n-butyl-2-nitratoethyl-nitramine). Other suitable plasticizers include DEGDN (diethyleneglycol dinitrate), TMETN (trimethylolethane trinitrate), and BTTN (butanetriol trinitrate). These plasticizers are used independently or in combination. Other fluoramino groups including bis-(2,2-ro-2-fluoroethyl) formal (FEFO) and bis-[2,2-bis(difluoramino)-5,5-dinitro-5-fluoropentoxy] methane (SYFO) could also incorporated into the formulations. In other embodiments of the present invention, the plasticizer include about 4 weight % of the formulations.
  • Iron oxide (Fe2O3), nano-sized is a suitable burn rate catalyst and is optional to exotic burn rate catalysts including superfine iron oxide, chromic oxide, catocene, or carboranes. In other embodiments aluminum oxide is also used. In embodiments of the present invention, the burn rate catalyst comprises about 1 weight % of the total metal composites. Tables I and II disclose a number of the formulations of the present invention.
    TABLE I
    Chemical Composition of Metal Composite Coated by Various Binders
    Plas-
    Reactive Metal Oxidizer Binder ticizer Catalyst
    80% H-5 14% AP, 11 μm 6% Viton ® None None
    60% H-5, 20% 14% AP, 11 μm 6% Viton ® None None
    Al/Mg
    alloy, 28 μm
    80% H-5 12% AP, 11 μm 6% Viton ® None 1% Fe2O 3,
    nano-sized
    74% H-5 20% AP, 11 μm 6% Viton ® None 1% Fe2O 3,
    nano-sized
    37% Ti, 44 μm 21% AP, 11 μm 6% None None
    37% B, 0.6-7 Nitrocellulose
    μm
    74% Ti—B, 21% AP, 11 μm 6% None None
    20 μm Nitrocellulose
    74% Mg—B, 21% AP, 11 μm 6% None None
    20 μm Nitrocellulose
    50% H-5 24% 20% AP, 11 μm 5% None 1% Fe2O3,
    Alex ® 0.2 μm Nitrocellulose nano-sized
    50% H-5 24% 20% AP, 11 μm 4% 4% 1% Fe2O3,
    Alex ® 0.2 μm Nitrocellulose FEFO nano-sized
    74% Alex ® 20% AP, 11 μm 5% None 1% Fe2O3,
    0.2 μm Nitrocellulose nano-sized
    40% Flake Al, 36% AP, 100 μm 4% Viton ® None None
    20% Al/Mg
    alloy

    Note:

    Al/Mg milled in batch MA020129-01,

    Ti—B milled in batch MA020317-01, and

    Mg—B milled in batch MA020319-01 at New Jersey Institute of Technology, Newark, New Jersey.
  • TABLE II
    Typical Composition of Castable PBX's Containing Reactive Metal and
    AP Oxidizer
    Reactive Plasticizer &
    Metal Oxidizer Binder High Explosive Catalyst
    20-40% 15-35% AP, 10-15% HTPB 30-55% HMX 4-6%
    11-100 μm
    Metal
    Composite Binder High Explosive Plasticizer
    40-60%* None 10-15% HTPB 30-45% HMX None
    or 30-50%
    HMX
    40-60%* None 10-15% LMA 30-45% None
    HMX
    30-55%* None 10-15% HTPB 35-60% CL-20 None
    20-24%* 15-35% AP 10-15% HTPB 30-55% HMX None

    Note:

    *metal composite contains oxidizer
  • The novel thermobaric explosives of the present invention are spherical particles of composite material containing high explosive, oxidizer, reactive metal and binder. Plasticizer and burn rate catalyst are added to manipulate performance. A method of making the novel thermobaric explosives described herein is disclosed in U.S. Pat. No. 5,750,921 issued to Chan et al. on May 12, 1998, hereby incorporated herein by reference.
  • In an embodiment of the present invention, a solid fuel-air explosive annular construction is used as shown in FIG. 1. In a typical annular construction, a cylindrical shell of solid fuel air explosive (SFAE) 22 surrounds the high explosive 21. As a matter of preference, the shapes of the high explosive charge are include, but not limited to spherically or cylindrically symmetric, to provide a uniform dispersion pattern. Solid metal casings 23 are typically pressed from reactive metal powder or metal composite (listed in Table 1) as SFAE. These solid metal casings are typically machined from stock into billets, but are also manufactured by other methods including casting or forging. The SFAE is then pressed into solid billets with a density (preferred to be 80-90% TMD) applicable to the particular use. The annular construction uses flake alumninum as the reactive metal. The SFAE billets are then placed in the warhead and the explosive is cast or pressed into place. The final SFAE fuel to explosive ratio is dependent upon the size and configuration of the warhead. PBX N112 consists of 89% HMX (high explosive) and 11% LMA (lauryl methacrylate). The PBX N112/reactive metal weight ratio includes the range of about 0.66 to about 1.45, or the ratio of about 1.
  • Embodiments of the compositions of the present invention are formed into a unicharge. The unicharge construct uses spherical aluminum as the reactive metal. Table II discloses ranges of ingredients for the formulations of the unicharge embodiment. As noted previously, a plasticizer and/or a burn rate catalyst are added to the formulations to tailor the formulations to particular needs. Although specific binders are listed, any of the binders previously noted are also used in the formulations. Similarly, any of the oxidizers previously noted are also substituted for AP and any of the high explosives previously noted are substituted for HMX.
  • Referring to FIG. 2, there is shown a plot illustrating the blast effectiveness of an explosive which includes a reactive metal of nano-meter sized metal particles. The metal particles used in the explosive have sizes of twenty nano-meters and two hundred nano-meters. For the first few micro-seconds the plot represented by the reference numeral 25 is virtually identical for the twenty nano-meter and two hundred nano-meter metal particles. After about 5-10 msec., the plots vary substantially. The plot for the twenty nano-meter metal particles (represented by the reference numeral 28) represents a blast effectiveness which is two times that of the two hundred nano-meter metal particles (represented by the reference numeral 26). As shown in FIG. 2, the time required for a complete release of energy can be reduced by substantially more than 50 msec and can be as much as 100 msec. Further, by using twenty nano-meter sized metal particles in the explosive device, the time required for total energy release is reduced to approximately 20 msec. which is genrally the maximum time during which total energy release by the explosive device should occur.
  • It should be understood that the examples and embodiments described herein are for illustrative purposes only and that various modifications or changes in light thereof will be suggested to persons skilled in the art and are to be included within the spirit and purview of this application and the scope of the appended claims.

Claims (17)

1. A metal composite comprising:
(a) about 60 to about 96 weight % of at least one nano-sized reactive metal, wherein each of said nano-sized reactive metals has an average particle size of approximetaly 20 nano-meters;
(b) about 4 to about 10 weight % of at least one binder; and
(c) about 0 to about 36 weight % of an oxidizer.
2. The metal composite of claim 1 wherein said at least one nano-sized reactive metal is selected from a group of nano-size reactive metals comprising nano-sized aluminum, nano-sized boron and nano-sized titanium.
3. The metal composite of claim 1 wherein said at least one nano-sized reactive metal is selected from a group of nano-size reactive metals comprizing nano-sized Al—Mg, Al—Mg—H, B—Mg, Al—B and Ti—B mixtures.
4. The metal composite of claim 1, wherein said binder comprises at least one of a copolymer of vinylidine fluoride hexafluoropropylene, nitrocellulose, glycidyl azide polymer (GAP) and Zeon.
5. The metal composite of claim 1, wherein said oxidizer is selected from the group comprising ammonium perchlorate, ammonium dinitramide and ammonium nitrate.
6. The metal composite of claim 1 wherein said metal composite provides for an explosiveness which maintains a relatively high pressure of approximately 30 to 60 psi for a time period of up to 50 msec.
7. The metal composite of claim 1 wherein the time required for a complete release of energy is reduced to approximately 20 msec by using said nano-sized reactive metals having said average particle size of approximetaly 20 nano-meters in said metal composite.
8. The metal composite of claim 7 wherein the time required for said complete release of energy is reduced by at least 50 msec by using said nano-sized reactive metals having said average particle size of approximetaly 20 nano-meters in said metal composite when compared to an explosive having 200 nano-meter metal particles contained therein.
9. A metal composite comprising:
(a) about 60 to about 96 weight % of at least one nano-sized reactive metal, wherein said at least one nano-sized reactive metal is selected from a group of nano-size reactive metals consisting of nano-sized aluminum, nano-sized boron, nano-sized magnesium, nano-sized titanium, nano-sized aluminum Born mixtures and nano-sized aluminum magnisium mixtures, each of said nano-sized reactive metals having an average particle size of about 20 nano-meters;
(b) about 4 to about 10 weight % of at least one binder; and
(c) about 0 to about 36 weight % of an oxidizer.
10. The metal composite of claim 9, wherein said binder comprises at least one of copolymer of vinylidine fluoride hexafluoropropylene, nitrocellulose, glycidyl azide polymer (GAP) and Zeon.
11. The metal composite of claim 9, wherein said oxidizer is selected from the group comprising ammonium perchlorate, ammonium dinitramide and ammonium nitrate.
12. The metal composite of claim 9, wherein said metal composite provides for an explosiveness which maintains a relatively high pressure of approximately 30 to 60 psi for a time period of up to 50 msec.
13. A metal composite comprising:
(a) about 60 to about 96 weight % of at least one nano-sized reactive metal, wherein said at least one nano-sized reactive metal is selected from a group of nano-size reactive metals consisting of nano-sized aluminum, nano-sized boron, nano-sized magnesium, nano-sized titanium, nano-sized aluminum Born mixtures and nano-sized aluminum magnisium mixtures, each of said nano-sized reactive metals having an average particle size of about 20 nano-meters;
(b) about 4 to about 10 weight % of at least one binder; and
(c) about 0 to about 36 weight % of an oxidizer, wherein the time required for a complete release of energy is reduced to approximately 20 msec by using said nano-sized reactive metals having said average particle size of approximetaly 20 nano-meters in said metal composite.
14. The metal composite of claim 13, wherein said binder comprises at least one of copolymer of vinylidine fluoride hexafluoropropylene, nitrocellulose, glycidyl azide polymer (GAP) and Zeon.
15. The metal composite of claim 13, wherein said oxidizer is selected from the group comprising ammonium perchlorate, ammonium dinitramide and ammonium nitrate.
16. The metal composite of claim 13, wherein said metal composite provides for an explosiveness which maintains a relatively high pressure of approximately 30 to 60 psi for a time period of up to 50 msec.
17. The metal composite of claim 13 wherein the time required for said complete release of energy is reduced by at least 50 msec by using said nano-sized reactive metals having said average particle size of approximetaly 20 nano-meters in said metal composite when compared to an explosive having 200 nano-meter metal particles contained therein.
US11/482,302 2002-12-23 2006-06-26 High energy blast explosives for confined spaces Pending US20070113939A1 (en)

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* Cited by examiner, † Cited by third party
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EP2170784A1 (en) * 2007-06-14 2010-04-07 BAE Systems Bofors AB Pyrotechnic priming charge comprising a porous material
US20100175367A1 (en) * 2007-06-08 2010-07-15 Thales Propellant device of enhanced performance
US20110030859A1 (en) * 2008-05-16 2011-02-10 Digital Solid State Propulsion, Llc Family of Metastable Intermolecular Composites Utilizing Energetic Liquid Oxidizers with NanoParticle Fuels In Sol-Gel Polymer Network
CN103159577A (en) * 2013-03-27 2013-06-19 北京理工大学 Underwater high-energy explosive containing ADN, and preparation method thereof
US20140090756A1 (en) * 2012-03-12 2014-04-03 University Of Central Florida Research Foundation, Inc. Compositions having aluminum particles dispersed in a continuous phase
EP2825516B1 (en) * 2012-03-12 2020-06-17 University Of Central Florida Research Foundation, Inc. Compositions having aluminum particles dispersed in a continuous phase
CN113603987A (en) * 2021-07-28 2021-11-05 中国工程物理研究院化工材料研究所 Modified aluminum/fluorine-containing polymer compound and preparation method thereof

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100175367A1 (en) * 2007-06-08 2010-07-15 Thales Propellant device of enhanced performance
US8257521B2 (en) * 2007-06-08 2012-09-04 Thales Propellant device of enhanced performance
EP2170784A1 (en) * 2007-06-14 2010-04-07 BAE Systems Bofors AB Pyrotechnic priming charge comprising a porous material
EP2170784A4 (en) * 2007-06-14 2012-05-30 Bae Systems Bofors Ab Pyrotechnic priming charge comprising a porous material
US20110030859A1 (en) * 2008-05-16 2011-02-10 Digital Solid State Propulsion, Llc Family of Metastable Intermolecular Composites Utilizing Energetic Liquid Oxidizers with NanoParticle Fuels In Sol-Gel Polymer Network
US8317953B2 (en) * 2008-05-16 2012-11-27 Digital Solid State Propulsion, Llc Family of metastable intermolecular composites utilizing energetic liquid oxidizers with nanoparticle fuels in sol-gel polymer network
US9573857B2 (en) * 2012-03-12 2017-02-21 University Of Central Florida Research Foundation, Inc. Compositions having aluminum particles dispersed in a continuous phase
US20140090756A1 (en) * 2012-03-12 2014-04-03 University Of Central Florida Research Foundation, Inc. Compositions having aluminum particles dispersed in a continuous phase
JP2015509906A (en) * 2012-03-12 2015-04-02 ユニヴァーシティ オブ セントラル フロリダ リサーチ ファウンデーション,インコーポレーテッドUniversity Of Central Florida Research Foundation, Inc. Composition having aluminum particles dispersed in continuous phase and method for forming the same
EP2825516B1 (en) * 2012-03-12 2020-06-17 University Of Central Florida Research Foundation, Inc. Compositions having aluminum particles dispersed in a continuous phase
CN103159577A (en) * 2013-03-27 2013-06-19 北京理工大学 Underwater high-energy explosive containing ADN, and preparation method thereof
CN113603987A (en) * 2021-07-28 2021-11-05 中国工程物理研究院化工材料研究所 Modified aluminum/fluorine-containing polymer compound and preparation method thereof
CN113603987B (en) * 2021-07-28 2022-07-26 中国工程物理研究院化工材料研究所 Modified aluminum/fluorine-containing polymer compound and preparation method thereof

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