GB2435645A - RDX density - Google Patents
RDX density Download PDFInfo
- Publication number
- GB2435645A GB2435645A GB0711449A GB0711449A GB2435645A GB 2435645 A GB2435645 A GB 2435645A GB 0711449 A GB0711449 A GB 0711449A GB 0711449 A GB0711449 A GB 0711449A GB 2435645 A GB2435645 A GB 2435645A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rdx
- solvent
- explosive
- less
- density
- 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.)
- Withdrawn
Links
- 239000013078 crystal Substances 0.000 claims abstract description 25
- 239000002360 explosive Substances 0.000 claims abstract description 23
- 238000005474 detonation Methods 0.000 claims description 6
- 239000000203 mixture Substances 0.000 abstract description 10
- 230000000977 initiatory effect Effects 0.000 abstract description 3
- 239000002904 solvent Substances 0.000 description 23
- 238000000034 method Methods 0.000 description 10
- 239000002245 particle Substances 0.000 description 8
- 239000000243 solution Substances 0.000 description 7
- 239000000463 material Substances 0.000 description 6
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 5
- 238000010304 firing Methods 0.000 description 5
- 239000003999 initiator Substances 0.000 description 5
- 230000015572 biosynthetic process Effects 0.000 description 4
- 239000011888 foil Substances 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- WFDIJRYMOXRFFG-UHFFFAOYSA-N Acetic anhydride Chemical compound CC(=O)OC(C)=O WFDIJRYMOXRFFG-UHFFFAOYSA-N 0.000 description 3
- ZMXDDKWLCZADIW-UHFFFAOYSA-N N,N-Dimethylformamide Chemical compound CN(C)C=O ZMXDDKWLCZADIW-UHFFFAOYSA-N 0.000 description 3
- TZRXHJWUDPFEEY-UHFFFAOYSA-N Pentaerythritol Tetranitrate Chemical compound [O-][N+](=O)OCC(CO[N+]([O-])=O)(CO[N+]([O-])=O)CO[N+]([O-])=O TZRXHJWUDPFEEY-UHFFFAOYSA-N 0.000 description 3
- 239000003990 capacitor Substances 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 238000001556 precipitation Methods 0.000 description 3
- 230000035945 sensitivity Effects 0.000 description 3
- IAZDPXIOMUYVGZ-UHFFFAOYSA-N Dimethylsulphoxide Chemical compound CS(C)=O IAZDPXIOMUYVGZ-UHFFFAOYSA-N 0.000 description 2
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 2
- 238000007599 discharging Methods 0.000 description 2
- 239000010419 fine particle Substances 0.000 description 2
- VKYKSIONXSXAKP-UHFFFAOYSA-N hexamethylenetetramine Chemical compound C1N(C2)CN3CN1CN2C3 VKYKSIONXSXAKP-UHFFFAOYSA-N 0.000 description 2
- 238000006396 nitration reaction Methods 0.000 description 2
- 229910017604 nitric acid Inorganic materials 0.000 description 2
- 238000001953 recrystallisation Methods 0.000 description 2
- 239000007858 starting material Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- PAWQVTBBRAZDMG-UHFFFAOYSA-N 2-(3-bromo-2-fluorophenyl)acetic acid Chemical compound OC(=O)CC1=CC=CC(Br)=C1F PAWQVTBBRAZDMG-UHFFFAOYSA-N 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- 125000004432 carbon atom Chemical group C* 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 239000008367 deionised water Substances 0.000 description 1
- 229910021641 deionized water Inorganic materials 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000009472 formulation Methods 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 235000010299 hexamethylene tetramine Nutrition 0.000 description 1
- 239000004312 hexamethylene tetramine Substances 0.000 description 1
- 150000002576 ketones Chemical class 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000005065 mining Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000003960 organic solvent Substances 0.000 description 1
- 239000008188 pellet Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B23/00—Compositions characterised by non-explosive or non-thermic constituents
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B21/00—Apparatus or methods for working-up explosives, e.g. forming, cutting, drying
- C06B21/0033—Shaping the mixture
- C06B21/0066—Shaping the mixture by granulation, e.g. flaking
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B25/00—Compositions containing a nitrated organic compound
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B25/00—Compositions containing a nitrated organic compound
- C06B25/18—Compositions containing a nitrated organic compound the compound being nitrocellulose present as 10% or more by weight of the total composition
- C06B25/22—Compositions containing a nitrated organic compound the compound being nitrocellulose present as 10% or more by weight of the total composition with a nitrated aromatic compound
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B25/00—Compositions containing a nitrated organic compound
- C06B25/34—Compositions containing a nitrated organic compound the compound being a nitrated acyclic, alicyclic or heterocyclic amine
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06C—DETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
- C06C5/00—Fuses, e.g. fuse cords
- C06C5/04—Detonating fuses
Landscapes
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Abstract
An explosive composition comprises RDX crystals typically having a crystal density of less than 1.80 g/cm3, a surface area greater than 1.15m<2>/g and an initiation threshold less than 100mJ.
Description
<p>RDX COMPOSITION</p>
<p>BACKGROUI4D The present invention relates generally to explosives, and more particularly to the explosive known as RDX.</p>
<p>The explosive hexahydro-l,3,5-trinitro-s-triazine is often referred to as RDX.</p>
<p>Two processes have been used commercially to manufacture RDX. The first is direct nitration, which produces type A RDX. In this process, hexamethylenetetraniine is reacted with nitric acid at 30 C or less. The direct nitration method is not widely used today for economic reasons. The second process, known as the Bachmann process, is currently the most common method used to manufacture RDX. It produces type B RDX. In this process, hexamethylenetetramine is reacted with nitric acid in the presence of ammonium nitrate and acetic anhydride.</p>
<p>The primary difference between the two types of RDX is that type A is essentially pure, while type B is contaminated with HMX. However, for practical purposes, both processes yield RDX of essentially identical utility. In both processes, the raw RDX is further purified and the crystal morphology is modified by recrystallization.</p>
<p>RDX is commonly manufactured in a wide range of particle sizes (grades) from microns to 600 microns in diameter by recrystallization. Recrystallized RDX may also be ground, for example in a fluid energy mill, to obtain finer particles ranging from 2 to 25 microns in diameter. However, all RDX commercially produced today consists of orthorhombic crystals with a density in the range of 1.80 -1.82 grams/cm3. This form of RDX has been designated as the a polymorph, or RDX(I). The exact crystal density of a given lot of RDX is a function of purity (i.e., HMX content), and the absence or presence of crystal defects and inclusions.</p>
<p>A 3 polymorph of RDX has been reported in the literature. The stability of 13-RDX is unknown and no measurements of physical properties or sensitivity have been reported other than the crystal morphology is dendritic.</p>
<p>RDX is an explosive material and therefore is used in a variety of applications in which controlled explosions are useful. In these applications, it is necessary to initiate the detonation of the RDX, and of course it is important to do so in a safe way.</p>
<p>A slapper detonator is a device that offers a relatively high degree of initiation safety. Slapper detonators function by rapidly discharging voltage through a low inductance circuit. The circuit comprises a high-voltage spark gap switch (typically 500 -3,500 volts), a high-voltage low-inductance capacitor (typically 500 -3,500 volts and 0.1 -0.2 j.tF), and an exploding-foil initiator (EFI) bridge. The entire circuit inductance is typically 20-50 nI-I, and sometimes less (1-20 nI-I). Discharging such a circuit causes a current of several thousand amperes to flow through the EFI bridge, which in turn causes the EFI bridge to explode. The exploding bridge then accelerates a polymeric flyer (typically a thin polyamide film) across a short gap, where it slaps a pellet of a secondary explosive, causing the secondary explosive to detonate.</p>
<p>Many explosives have been detonated in a laboratory setting by slapper detonators, such as FINS, PETN, CL-20, TNT, RDX, HMX, and various formulations made from such explosives. However, such laboratory initiation systems typically function at high voltages with large capacitors and discharge energies of 250 rnJ to 1,225 mJ. Such systems are generally unsuitable for use outside the laboratory. To be useful outside the laboratory, experience has shown that it is desirable to significantly reduce the firing voltage and capacitor size (firing energy) of the circuit. While this can be accomplished to some degree by designing the electrical firing circuit to be more efficient, ultimately the minimum firing energy is controlled by the sensitivity of the explosive.</p>
<p>The current state of the art is the low-energy foil initiator (LEFT) These devices typically function with firing energies below 100 mJ. To this end, explosives have been developed that have fine particle size and high surface area, such as HNS-JV, PETN, and CL-20, which can be initiated with less than 100 mJ. However, each of these explosives has significant problems. HNS-IV is difficult to manufacture and purify, and therefore is expensive. PETN has excellent sensitivity and an acceptable price, but has marginal thermal stability for non-laboratory applications. CL-20 is expensive and cannot be recrystallized to a very small particle size. It is therefore just barely sensitive enough for a LEFI application.</p>
<p>There is a need for new explosive materials that can be initiated by LEFI devices, and that overcome at least some of the above-described problems.</p>
<p>SUMMARY OF THE INVENTION</p>
<p>The present invention resides in RDX crystals having a crystal density of less than 1.80 g/cm3.</p>
<p>BRIEF DESCRIPTION OF THE DRAWINGS</p>
<p>Figure 1 is an enlarged illustration of type B RDX particles.</p>
<p>Figure 2 is an enlarged illustration of RDX particles of the present invention.</p>
<p>Figure 3 is a schematic diagram of a perforating system of the present invention.</p>
<p>DESCRIPTION OF ILLUSTRATIVE EMBODIMENTS</p>
<p>The present invention relates to a novel form of RDX that can be used in the perforation of well casing, among other applications.</p>
<p>The production of the novel form of RDX begins with a particulate RDX composition. This starting composition contains primarily RDX (e.g., at least about 90 wt% RDX on a dry solids basis, and in some embodiments at least about 99 wt% RDX), but it can also contain smaller amounts of other explosive or non-explosive substances, such as HMIX. Type B RDX is one suitable starting material.</p>
<p>The RDX is dissolved in a first solvent to form a first solution. RDX should be soluble in this first solvent to an extent of greater than I g RDX/1 00 g solvent. In various embodiments of the invention, the solubility of RDX in the first solvent is greater than 5 g/lOOg, 10 g/IOOg, or 25 gf 100g. (All solubility figures in this patent are at room temperature unless otherwise stated.) The concentration of RDX in the solution will generally be about 1-50 wt%, although higher or lower concentrations can be used in some situations.</p>
<p>The first solvent will typically be an organic solvent, for example one having about 2-10 carbon atoms. Ketones are one group of suitable solvents. Specific examples of suitable first solvents include acetone, dimethylsulfoxide, and dimethylformamide.</p>
<p>A second solvent is then added to the solution, in order to cause "crash" precipitation of RDX particles. The second solvent is miscible with the first solvent, but RDX is much less soluble in the second solvent than in the first solvent. In various embodiments of the invention, RDX is soluble in the second solvent to an extent no greater than ig of RDX/lOOg of the second solvent, or in some cases no greater than 0. Ig/lOOg. Suitable examples of second solvents include water and various dilute aqueous solutions.</p>
<p>The second solvent can be added in an excess compared to the volume of the first solvent in the solution. For example, the second solvent can be added in a volume that is about 2-10 times greater than the volume of the first solvent. Even more of the second solvent can be used, although it may be economically undesirable in many cases.</p>
<p>In contrast, if the amount of the second solvent used is too small, the resulting crystals will not have the desired properties and will not function as an EFI explosive.. The solution can be agitated during and/or after the addition of the second solvent.</p>
<p>The addition of the second solvent will cause precipitation of RDX particles.</p>
<p>The particles can be recovered, for example by filtration, and then washed and dried.</p>
<p>The fmal RDX composition can be essentially pure RDX, or it can contain smaller amounts of other substances, such as HMX. In contrast to the RDX that has been commercially available in the past, the RDX has a crystal density of less than 1.80 glcm3. In some cases, the RDX has a crystal density of about 1.65-1.73 g/cm3. In some embodiments of the invention, the RDX has a surface area of greater than about 1.15 m2/g.</p>
<p>The detonation of RDX produced by the above-described process can generally be initiated with less energy than what is required to initiate previously-known RDX compositions. In some embodiments of the invention, detonation of the RDX can be initiated with less than about 1 OOmJ, or in some cases, less than about 75 mJ.</p>
<p>Figure 1 shows a sample of type B RDX at 1 OOx magnification, while Figure 2 shows a sample of the RDX of the present invention at 790x magnification.</p>
<p>The RDX composition of the present invention can be used in a variety of applications. For example, it can be used in perforating the casing of subterranean wells, mining, construction blasting, and many other applications that are well known in the explosive industry.</p>
<p>Figure 3 shows a schematic view of the use of the RDX composition to perforate a well casing. A borehole 10 has been drilled down from the surface of the earth into a subterranean formation 12. The borehole has been lined with casing 14, which generally takes the form of a cylindrical pipe. At some depth or depths in the borehole, the surrounding formation 12 contains oil and/or gas. In order for the oil and/or gas to pass from the formation into the borehole and up to the surface, it is necessary to perforate the casing. This can be done with a perforating gun 16, which can be lowered into the well to the desired depth on a wireline 18 or using other means that are known in the oil industry.</p>
<p>The perforating gun 16 comprises a plurality of shaped charges 20, each of which contains an explosive material. This explosive material can be the RDX produced as described above, alone or in combination with other materials that are suitable for use in an explosive composition. Detonation of the explosive material in the shaped charge 20 can be initiated by a low-energy foil initiator 22. When an electrical signal is sent via a control line from a control device at the surface (not shown in Fig. 3), the initiator 22 causes the detonation of the shaped charge 20. The explosive force from the shaped charge 20 is directed primarily horizontally to the left in Fig. 3, such that a perforation is formed in the casing, allowing oil and gas in the formation to flow into the borehole.</p>
<p>It should be understood that the arrangement shown in Fig. 3 is only one example of how the RDX of the present invention could be used in the perforation of well casing.</p>
<p>Specific embodiments of the present invention can be further understood from the following example.</p>
<p>Example 1</p>
<p>RDX crystals were prepared by crash precipitation. Type B RDX was dissolved in acetone to make a 10% by weight solution. A large excess of deionized water was added to this solution with vigorous stirring to precipitate fine particle size RDX. The precipitated RDX crystals were filtered from the liquid and washed. The resulting RDX was dried at 50-55 C overnight in a drying oven. The measured BET surface area of the precipitated RDX was in excess of 1.2 m2/g. When examined by light microscope, the RDX crystals appeared to be polycrystalline and orthorhombic. However, when the crystal density of the crash-precipitated RDX was checked by helium pyconometer, the crystal density was found to be 1.69 g/tn, which is significantly different than the starting material (Ca. 1.80-1.82 g/cm3).</p>
<p>The RDX crystals were successftilly detonated in a low-energy exploding foil initiator (LEFI) at 72 mJ (1300 volts, 0.085.tF).</p>
<p>The preceding description is not intended to be an exhaustive list of every possible embodiment of the present invention. Persons skilled in the art will recognize that modifications could be made to the embodiments described above which would remain within the scope of the following claims.</p>
Claims (1)
- <p>CLAIMS</p><p>I. RDX crystals having a crystal density of less than 1.80 g/cm3.</p><p>2. The RDX crystals of claim 1, wherein the RDX crystals have a surface area of greater than 1.15 m2/g.</p><p>3. The RDX crystals of claim 1, wherein detonation of the RDX crystals can be initiated with less than 100 mJ.</p><p>4. An explosive comprising RDX crystals in accordance with any preceding claim.</p>
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/160,021 US20060272756A1 (en) | 2005-06-06 | 2005-06-06 | RDX Composition and Process for Its Manufacture |
GB0607418A GB2426974B (en) | 2005-06-06 | 2006-04-13 | RDX composition and process |
Publications (2)
Publication Number | Publication Date |
---|---|
GB0711449D0 GB0711449D0 (en) | 2007-07-25 |
GB2435645A true GB2435645A (en) | 2007-09-05 |
Family
ID=36571748
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0607418A Expired - Fee Related GB2426974B (en) | 2005-06-06 | 2006-04-13 | RDX composition and process |
GB0711449A Withdrawn GB2435645A (en) | 2005-06-06 | 2007-06-14 | RDX density |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0607418A Expired - Fee Related GB2426974B (en) | 2005-06-06 | 2006-04-13 | RDX composition and process |
Country Status (4)
Country | Link |
---|---|
US (1) | US20060272756A1 (en) |
FR (1) | FR2887543B1 (en) |
GB (2) | GB2426974B (en) |
RU (1) | RU2342351C2 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8051775B2 (en) | 2008-07-18 | 2011-11-08 | Schlumberger Technology Corporation | Detonation to igniter booster device |
US8226782B2 (en) | 2008-07-10 | 2012-07-24 | Schlumberger Technology Corporation | Application of high temperature explosive to downhole use |
US8359977B2 (en) | 2008-12-27 | 2013-01-29 | Schlumberger Technology Corporation | Miniature shaped charge for initiator system |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060219341A1 (en) * | 2005-03-30 | 2006-10-05 | Johnston Harold E | Heavy metal free, environmentally green percussion primer and ordnance and systems incorporating same |
US8641842B2 (en) | 2011-08-31 | 2014-02-04 | Alliant Techsystems Inc. | Propellant compositions including stabilized red phosphorus, a method of forming same, and an ordnance element including the same |
US7857921B2 (en) * | 2006-03-02 | 2010-12-28 | Alliant Techsystems Inc. | Nontoxic, noncorrosive phosphorus-based primer compositions |
US8540828B2 (en) | 2008-08-19 | 2013-09-24 | Alliant Techsystems Inc. | Nontoxic, noncorrosive phosphorus-based primer compositions and an ordnance element including the same |
CA2942312C (en) | 2007-02-09 | 2019-05-28 | Vista Outdoor Operations Llc | Non-toxic percussion primers and methods of preparing the same |
US8192568B2 (en) | 2007-02-09 | 2012-06-05 | Alliant Techsystems Inc. | Non-toxic percussion primers and methods of preparing the same |
WO2008098302A1 (en) * | 2007-02-16 | 2008-08-21 | Orica Explosives Technology Pty Ltd | Method of communication at a blast site, and corresponding blasting apparatus |
US8002917B2 (en) | 2009-02-09 | 2011-08-23 | The United States Of America As Represented By The Secretary Of The Army | Adjusting yield of a manufacturing process for energetic compounds through solubility modification |
US8206522B2 (en) | 2010-03-31 | 2012-06-26 | Alliant Techsystems Inc. | Non-toxic, heavy-metal free sensitized explosive percussion primers and methods of preparing the same |
RU2449976C1 (en) * | 2010-09-13 | 2012-05-10 | Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" - Госкорпорация "Росатом" | Method of changing crystal shape of explosive substance |
CN103772077B (en) * | 2014-01-24 | 2016-08-17 | 四川省南部永生化工有限责任公司 | A kind of defective explosive processing means |
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RU2204508C1 (en) * | 2002-04-22 | 2003-05-20 | Денисов Иван Васильевич | Method of breaking fragments of space debris |
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US3181463A (en) * | 1961-03-17 | 1965-05-04 | Gen Precision Inc | Explosive device containing charge of elongated crystals and an exploding bridgewire |
US3266957A (en) * | 1964-09-24 | 1966-08-16 | Richard H Stresau | Booster explosive of ultrafine desensitized cyclotrimethylene-trinitramine and method of preparing same |
US3754061A (en) * | 1971-08-13 | 1973-08-21 | Du Pont | Method of making spheroidal high explosive particles having microholes dispersed throughout |
DE2756335C2 (en) * | 1977-12-17 | 1982-06-16 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V., 8000 München | Process for the production of crystalline nitroguanidine of high bulk density |
SE451718B (en) * | 1984-04-04 | 1987-10-26 | Nobel Kemi Ab | SET TO RECRISTALIZE THE EXPLOSIVES OCTOGEN AND HEXOGEN |
US4650617A (en) * | 1985-06-26 | 1987-03-17 | Morton Thiokol Inc. | Solvent-free preparation of gun propellant formulations |
US5360478A (en) * | 1989-10-16 | 1994-11-01 | Phasex Corporation | Gas anti-solvent recrystallization process |
KR940004638B1 (en) * | 1991-03-06 | 1994-05-27 | 국방과학연구소 | Composite powder of condensed type using the adhesive agent with ethylene acetic vinyl resin |
US5389263A (en) * | 1992-05-20 | 1995-02-14 | Phasex Corporation | Gas anti-solvent recrystallization and application for the separation and subsequent processing of RDX and HMX |
US5359936A (en) * | 1993-03-08 | 1994-11-01 | Regents Of The University Of California | Non-detonable explosive simulators |
US5284995A (en) * | 1993-03-08 | 1994-02-08 | The United States Of America As Represented By The Secretary Of The Army | Method to extract and recover nitramine oxidizers from solid propellants using liquid ammonia |
US6173650B1 (en) * | 1999-06-30 | 2001-01-16 | The United States Of America As Represented By The Secretary Of The Navy | MEMS emergetic actuator with integrated safety and arming system for a slapper/EFI detonator |
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-
2005
- 2005-06-06 US US11/160,021 patent/US20060272756A1/en not_active Abandoned
-
2006
- 2006-04-13 GB GB0607418A patent/GB2426974B/en not_active Expired - Fee Related
- 2006-05-11 FR FR0604320A patent/FR2887543B1/en not_active Expired - Fee Related
- 2006-06-05 RU RU2006119613/02A patent/RU2342351C2/en not_active IP Right Cessation
-
2007
- 2007-06-14 GB GB0711449A patent/GB2435645A/en not_active Withdrawn
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RU2204508C1 (en) * | 2002-04-22 | 2003-05-20 | Денисов Иван Васильевич | Method of breaking fragments of space debris |
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"Explosive Chemistry"; Island Pyrochemical Industries (IPI) found at Internet URL:http://www.islandgroup.com/ExplosiveChemistry.html * |
"Studies on Explosive-Thermal-Mechanical Properties of RDX Based Sheet Explosive Composition Using Polyurethane and Viton as binders" - Jangid, Nath, Asthana & Rao / High Energy Materials Research Laboratory, India. Found at Internet URL:http://www.ncl-india.org/macro2006/upload/CD-1/macro/Lecture/S * |
Internet URL:http://en.wikipedia.org/wiki/RDX * |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8226782B2 (en) | 2008-07-10 | 2012-07-24 | Schlumberger Technology Corporation | Application of high temperature explosive to downhole use |
US8051775B2 (en) | 2008-07-18 | 2011-11-08 | Schlumberger Technology Corporation | Detonation to igniter booster device |
US8359977B2 (en) | 2008-12-27 | 2013-01-29 | Schlumberger Technology Corporation | Miniature shaped charge for initiator system |
Also Published As
Publication number | Publication date |
---|---|
US20060272756A1 (en) | 2006-12-07 |
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GB0607418D0 (en) | 2006-05-24 |
RU2342351C2 (en) | 2008-12-27 |
GB2426974A (en) | 2006-12-13 |
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