GB2435645A - RDX density - Google Patents

RDX density Download PDF

Info

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Withdrawn
Application number
GB0711449A
Other versions
GB0711449D0 (en
Inventor
Philip Kneisl
Karri A Brock
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.)
Gemalto Terminals Ltd
Schlumberger Holdings Ltd
Original Assignee
Gemalto Terminals Ltd
Schlumberger Holdings Ltd
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 Gemalto Terminals Ltd, Schlumberger Holdings Ltd filed Critical Gemalto Terminals Ltd
Publication of GB0711449D0 publication Critical patent/GB0711449D0/en
Publication of GB2435645A publication Critical patent/GB2435645A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B23/00Compositions characterised by non-explosive or non-thermic constituents
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B21/00Apparatus or methods for working-up explosives, e.g. forming, cutting, drying
    • C06B21/0033Shaping the mixture
    • C06B21/0066Shaping the mixture by granulation, e.g. flaking
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B25/00Compositions containing a nitrated organic compound
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B25/00Compositions containing a nitrated organic compound
    • C06B25/18Compositions containing a nitrated organic compound the compound being nitrocellulose present as 10% or more by weight of the total composition
    • C06B25/22Compositions 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
    • 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
    • C06CDETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
    • C06C5/00Fuses, e.g. fuse cords
    • C06C5/04Detonating 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)

  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>
GB0711449A 2005-06-06 2007-06-14 RDX density Withdrawn GB2435645A (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2204508C1 (en) * 2002-04-22 2003-05-20 Денисов Иван Васильевич Method of breaking fragments of space debris

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US7214509B2 (en) * 2003-06-30 2007-05-08 University Of Iowa Research Foundation Methods and compositions for degradation of nitroaromatic and nitramine pollutants

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2204508C1 (en) * 2002-04-22 2003-05-20 Денисов Иван Васильевич Method of breaking fragments of space debris

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
"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)

* Cited by examiner, † Cited by third party
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
FR2887543A1 (en) 2006-12-29
RU2006119613A (en) 2007-12-10
GB0711449D0 (en) 2007-07-25
GB2426974B (en) 2008-01-23
FR2887543B1 (en) 2009-04-17
GB0607418D0 (en) 2006-05-24
RU2342351C2 (en) 2008-12-27
GB2426974A (en) 2006-12-13

Similar Documents

Publication Publication Date Title
US20060272756A1 (en) RDX Composition and Process for Its Manufacture
US3181463A (en) Explosive device containing charge of elongated crystals and an exploding bridgewire
US10151569B2 (en) Initiator having an explosive substance of a secondary explosive
US3037452A (en) Booster for relatively insensitive explosives
US8226782B2 (en) Application of high temperature explosive to downhole use
WO2015116662A1 (en) Collapse initiated explosive pellet
AU2018281438B2 (en) Explosive body for nanodiamond synthesis
US9850181B1 (en) Single-step production method for nano-sized energetic cocrystals by bead milling and products thereof
Roeske et al. Cutting and machining energetic materials with a femtosecond laser
CN113862754B (en) Preparation method of green ton sense nano array initiating explosive
IL35361A (en) Liquid explosive
US9701592B1 (en) Single-step production method for nano-sized energetic cocrystals by bead milling and products thereof
EP2945919B1 (en) Explosive composition for use in telescopically expanding non-lethal training ammunition
Maksimowski et al. Comparison of the Crystals Obtained by Precipitation of CL‐20 with Different Chemical Purity
Boileau et al. Explosives
US3317360A (en) Preparation of electric blasting cap mixture containing amorphous boron and lead oxide
Brogle et al. Environmentally friendly recycling of hexal in medium caliber ammunition in industrial scale
JP2008189515A (en) Desensitized explosive composition, and method for producing the same
SE446179B (en) WAY TO FLEGATIZATE FAST EXPLOSIVE SUBSTANCES
Xu et al. Effect of purity on the properties of ultrafine HNS
Liu et al. Pentaerythritol Tetranitrate
RU2060449C1 (en) Casing explosive device
Lanzerotti et al. Mechanical behavior of energetic materials during high acceleration in an ultracentrifuge
CN116514664A (en) Hexanitrostilbene purification process
US3431156A (en) Complex crystalline picrate explosive containing entrapped amounts of lead azide

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)