EP1241150B1 - Process for producing mouldable, plastic-bound explosives or rocket propellants - Google Patents
Process for producing mouldable, plastic-bound explosives or rocket propellants Download PDFInfo
- Publication number
- EP1241150B1 EP1241150B1 EP01129902A EP01129902A EP1241150B1 EP 1241150 B1 EP1241150 B1 EP 1241150B1 EP 01129902 A EP01129902 A EP 01129902A EP 01129902 A EP01129902 A EP 01129902A EP 1241150 B1 EP1241150 B1 EP 1241150B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- metal powder
- plastic
- explosive
- groups
- rocket propellants
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000002360 explosive Substances 0.000 title claims description 23
- 239000004033 plastic Substances 0.000 title claims description 9
- 239000003380 propellant Substances 0.000 title claims description 4
- 238000000034 method Methods 0.000 title claims 4
- 239000000843 powder Substances 0.000 claims description 19
- 229910052751 metal Inorganic materials 0.000 claims description 18
- 239000002184 metal Substances 0.000 claims description 18
- 239000000203 mixture Substances 0.000 claims description 10
- IJOOHPMOJXWVHK-UHFFFAOYSA-N chlorotrimethylsilane Chemical compound C[Si](C)(C)Cl IJOOHPMOJXWVHK-UHFFFAOYSA-N 0.000 claims description 8
- 238000004519 manufacturing process Methods 0.000 claims description 4
- 150000003254 radicals Chemical class 0.000 claims description 4
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 4
- 239000005051 trimethylchlorosilane Substances 0.000 claims description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 2
- 125000000217 alkyl group Chemical group 0.000 claims description 2
- 150000005840 aryl radicals Chemical class 0.000 claims description 2
- 229910052804 chromium Inorganic materials 0.000 claims description 2
- 239000011651 chromium Substances 0.000 claims description 2
- 229910052750 molybdenum Inorganic materials 0.000 claims description 2
- 239000011733 molybdenum Substances 0.000 claims description 2
- 229910052758 niobium Inorganic materials 0.000 claims description 2
- 239000010955 niobium Substances 0.000 claims description 2
- 238000009738 saturating Methods 0.000 claims description 2
- 229910052715 tantalum Inorganic materials 0.000 claims description 2
- 229910052720 vanadium Inorganic materials 0.000 claims description 2
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims description 2
- 150000002739 metals Chemical class 0.000 claims 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims 1
- 125000001181 organosilyl group Chemical group [SiH3]* 0.000 claims 1
- 229920006395 saturated elastomer Polymers 0.000 claims 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims 1
- 229910052721 tungsten Inorganic materials 0.000 claims 1
- 239000010937 tungsten Substances 0.000 claims 1
- 239000007787 solid Substances 0.000 description 5
- 239000002245 particle Substances 0.000 description 3
- XTFIVUDBNACUBN-UHFFFAOYSA-N 1,3,5-trinitro-1,3,5-triazinane Chemical compound [O-][N+](=O)N1CN([N+]([O-])=O)CN([N+]([O-])=O)C1 XTFIVUDBNACUBN-UHFFFAOYSA-N 0.000 description 2
- 239000000028 HMX Substances 0.000 description 2
- OFBQJSOFQDEBGM-UHFFFAOYSA-N Pentane Chemical compound CCCCC OFBQJSOFQDEBGM-UHFFFAOYSA-N 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 230000009969 flowable effect Effects 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 125000002887 hydroxy group Chemical group [H]O* 0.000 description 2
- 239000012948 isocyanate Substances 0.000 description 2
- 150000002513 isocyanates Chemical group 0.000 description 2
- UZGLIIJVICEWHF-UHFFFAOYSA-N octogen Chemical compound [O-][N+](=O)N1CN([N+]([O-])=O)CN([N+]([O-])=O)CN([N+]([O-])=O)C1 UZGLIIJVICEWHF-UHFFFAOYSA-N 0.000 description 2
- 229920000642 polymer Polymers 0.000 description 2
- 229920002121 Hydroxyl-terminated polybutadiene Polymers 0.000 description 1
- 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 1
- 239000000026 Pentaerythritol tetranitrate Substances 0.000 description 1
- -1 alkyl radicals Chemical class 0.000 description 1
- 239000003963 antioxidant agent Substances 0.000 description 1
- 230000003078 antioxidant effect Effects 0.000 description 1
- 239000007767 bonding agent Substances 0.000 description 1
- 125000003178 carboxy group Chemical group [H]OC(*)=O 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- KPUWHANPEXNPJT-UHFFFAOYSA-N disiloxane Chemical compound [SiH3]O[SiH3] KPUWHANPEXNPJT-UHFFFAOYSA-N 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000009472 formulation Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- ZYTNDGXGVOZJBT-UHFFFAOYSA-N niobium Chemical compound [Nb].[Nb].[Nb] ZYTNDGXGVOZJBT-UHFFFAOYSA-N 0.000 description 1
- 229960004321 pentaerithrityl tetranitrate Drugs 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000012216 screening Methods 0.000 description 1
- WTKKCYNZRWIVKL-UHFFFAOYSA-N tantalum Chemical compound [Ta+5] WTKKCYNZRWIVKL-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
- C06B45/18—Compositions or products which are defined by structure or arrangement of component of product comprising a coated component
- C06B45/30—Compositions or products which are defined by structure or arrangement of component of product comprising a coated component the component base containing an inorganic explosive or an inorganic thermic component
- C06B45/32—Compositions or products which are defined by structure or arrangement of component of product comprising a coated component the component base containing an inorganic explosive or an inorganic thermic component the coating containing an organic compound
-
- 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
- C06B21/0008—Compounding the ingredient
- C06B21/0025—Compounding the ingredient the ingredient being a polymer bonded explosive or thermic component
Definitions
- the invention relates to a method for producing pourable plastic bonded explosive charges or rocket fuels.
- Plastic-bonded explosive charges have a relatively high insensitivity despite a high active power on. They consist of reaction polymers in which crystalline before hardening Explosives, such as octogen, hexogen, pentaerythritol tetranitrate, etc., are incorporated. there the polymer content is about 10 to 20 wt .-%.
- a problem in the production of plastic-bound explosive charges is that with increasing Solid content, i. with increasing content of explosive, the viscosity of the mixture can increase so that a pouring of this mixture is impossible.
- the theoretical Limit for a flowable mixture is 92 wt .-%. However, it has been shown that the practical limit for flowable mixtures is about 90 wt .-%.
- There are also explosive charges with such a high solids content only pourable when the particle sizes of the for the Explosive charge used explosive crystals within a given diameter interval lie, so that a relatively expensive screening of grain fractions is required.
- the solids content and thus the performance increase plastic-bound explosive charges without increasing the viscosity, that 0.1 to 10 wt .-% of the solid when mixed with the curable plastic binder as the finest grain with a mean grain size less than 25 microns, preferably less than 8 microns added becomes.
- the invention is based on the object, a method for producing insensitive pourable plastic bonded explosive charges or rocket propellants with a high (e.g., 90%) solids content, with an increase the viscosity by polar deposited on the metal surface of the metal powder Groups is avoided.
- R organic radical
- the polar groups can no longer react with the isocyanates and the specific surface area of the respective metal powder decreases.
- the viscosity of the explosive charge decreases.
- Suitable organic radicals are all alkyl and aryl radicals, the alkyl radicals being more reactive.
- tungsten powder particles size between 3 and 5 microns
- a solution of 900 g of pentane and 20 g of trimethylchlorosilane were placed in a solution of 900 g of pentane and 20 g of trimethylchlorosilane and stirred for 5 minutes. Subsequently, the tungsten powder was filtered off and dried in a drying oven. While the specific surface before treatment with Me3SiCl was 0.1978 m 2 / g, after treatment it was only 0.1880 m 2 / g, which subsequently led to a reduction of the viscosity of the explosive mixture from approx. 600 - 800 Pas to approx 400 Pas led.
- the preparation of the explosive charges according to the invention can be carried out, for example, by means of the following typical formulations: 80-88% by weight Crystalline explosive, eg RDX or HMX 10-20% by weight Binder, eg HTPB 5-10% by weight softener 0.01-02% by weight bonding agent 0.05-05% by weight coating aids 0.1-1.0% by weight antioxidant 0.1-10% by weight metal powder
- the grain size of the respective metal powder should be between 0.1 and 5 ⁇ m lie.
Landscapes
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Processes Of Treating Macromolecular Substances (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
- Powder Metallurgy (AREA)
- Lubricants (AREA)
- Manufacture Of Metal Powder And Suspensions Thereof (AREA)
Description
Die Erfindung betrifft ein Verfahren zur Herstellung gießfähiger kunststoffgebundener Sprengladungen oder Raketentreibstoffe.The invention relates to a method for producing pourable plastic bonded explosive charges or rocket fuels.
Kunststoffgebundene Sprengladungen weisen trotz einer hohen Wirkleistung eine relativ hohe Unempfindlichkeit auf. Sie bestehen aus Reaktionspolymeren, in die vor der Aushärtung kristalline Explosivstoffe, wie Octogen, Hexogen, Pentaerythrittetranitrat etc., eingearbeitet werden. Dabei beträgt der Polymeranteil etwa 10 bis 20 Gew.-%.Plastic-bonded explosive charges have a relatively high insensitivity despite a high active power on. They consist of reaction polymers in which crystalline before hardening Explosives, such as octogen, hexogen, pentaerythritol tetranitrate, etc., are incorporated. there the polymer content is about 10 to 20 wt .-%.
Ein Problem bei der Herstellung kunststoffgebundener Sprengladungen besteht darin, daß mit steigendem Feststoffanteil, d.h. mit zunehmendem Anteil an Explosivstoff, die Viskosität der Mischung so zunehmen kann, daß ein Gießen dieser Mischung unmöglich wird. Die theoretische Grenze für ein fließfähiges Gemisch liegt bei 92 Gew.-%. Es hat sich allerdings gezeigt, daß die praktische Grenze für fließfähige Gemische bei ca. 90 Gew.-% liegt. Außerdem sind Sprengladungen mit einem derart hohen Feststoffanteil nur dann gießbar, wenn die Korngrößen der für die Sprengladung verwendeten Explosivstoffkristalle innerhalb eines vorgegebenen Durchmesserintervalles liegen, so daß ein relativ kostenintensives Aussieben von Kornfraktionen erforderlich ist.A problem in the production of plastic-bound explosive charges is that with increasing Solid content, i. with increasing content of explosive, the viscosity of the mixture can increase so that a pouring of this mixture is impossible. The theoretical Limit for a flowable mixture is 92 wt .-%. However, it has been shown that the practical limit for flowable mixtures is about 90 wt .-%. There are also explosive charges with such a high solids content only pourable when the particle sizes of the for the Explosive charge used explosive crystals within a given diameter interval lie, so that a relatively expensive screening of grain fractions is required.
Aus der DE-C-38 04 396 ist es bereits bekannt, den Feststoffanteil und damit die Leistung kunststoffgebundener Sprengladungen ohne Zunahme der Viskosität dadurch zu erhöhen, daß 0,1 bis 10 Gew.-% des Feststoffes beim Mischen mit dem aushärtbaren Kunststoffbinder als Feinstkorn mit einer mittleren Korngröße kleiner 25 µm, vorzugsweise kleiner 8 µm, zugegeben wird.From DE-C-38 04 396 it is already known, the solids content and thus the performance increase plastic-bound explosive charges without increasing the viscosity, that 0.1 to 10 wt .-% of the solid when mixed with the curable plastic binder as the finest grain with a mean grain size less than 25 microns, preferably less than 8 microns added becomes.
Die Anmelderin hat in der veröffentlichten Patentanmeldung EP-A-1211232 bereits vor geschlagen, der jeweiligen Sprengladung 0,1 bis 10 Gew.-% feinstkörniges Vanadin-, Niob-, Tantal-, Chrom-, Molybdän- oder Wolfram-Pulver oder eine Mischung aus zwei oder mehreren derartigen Pulvern zuzusetzen, wobei die Pulverkörner eine im wesentlichen sphärische Form aufweisen sollen. Bei Verwendung dieser Metallpulver, die aufgrund der sphärischen Form der Pulverkörner eine sehr kleine spezifische Oberfläche aufweisen, hat sich überraschenderweise gezeigt, daß sie wie flüssige Schmiermittel zwischen den grobkörnigeren Sprengstoffpartikeln wirken (Tribologischer Effekt), so daß sich relativ niedrige Viskositäten ergeben.The Applicant has already published in published patent application EP-A-1211232 0.1-0.0% by weight of very fine-grained vanadium, the respective explosive charge, Niobium, tantalum, chromium, molybdenum or tungsten powder or a mixture from two or more such powders, wherein the powder grains a should have substantially spherical shape. When using this metal powder, due to the spherical shape of the powder grains a very small specific Have surface, has surprisingly been found that they like liquid Lubricant between the coarse-grained explosive particles act (Tribological Effect), resulting in relatively low viscosities.
Untersuchungen der Anmelderin haben ergeben, daß beim Einbringen der Metallpulver in die kunststoffgebundenen Sprengladungen bzw. Raketentreibstoffe die Viskositätsverminderung noch nicht optimal ist. Denn an der Oberfläche der Metallpulver sind häufig polare Gruppen angelagert, die mit den Isocyanaten der kunststoffgebundenen Sprengladungen bzw. mit den Raketentreibstoffen reagieren, was dann zu einem Erhöhen der Viskosität der entsprechenden Mischung führen kann. Dieses gilt insbesondere für die an der Oberfläche durch Einwirkung von Luftfeuchtigkeit angelagerten OH-Gruppen. Aber auch andere an den Metalloberflächen angelagerte polare Gruppen (z.B. Carboxyl-Gruppen) können zu einer Erhöhung der Viskosität führen.Investigations by the applicant have shown that when introducing the metal powder in the plastic-bound explosive charges or rocket propellants, the viscosity reduction not yet optimal. Because on the surface of the metal powder are often polar groups attached to the isocyanates of the plastic-bound Explosive charges or react with the rocket fuels, which then to a Increasing the viscosity of the corresponding mixture can result. This is true in particular for those deposited on the surface by the action of atmospheric moisture OH groups. But also other attached to the metal surfaces Polar groups (e.g., carboxyl groups) can increase viscosity to lead.
Der Erfindung liegt die Aufgabe zugrunde, ein Verfahren zur Herstellung unempfindlicher gießfähiger kunststoffgebundener Sprengladungen oder Raketentreibstoffe mit einem hohen (z.B. 90 %-igen) Feststoffanteil anzugeben, mit dem eine Erhöhung der Viskosität durch an der Metalloberfläche der Metallpulver angelagerte polare Gruppen vermieden wird.The invention is based on the object, a method for producing insensitive pourable plastic bonded explosive charges or rocket propellants with a high (e.g., 90%) solids content, with an increase the viscosity by polar deposited on the metal surface of the metal powder Groups is avoided.
Diese Aufgabe wird erfindungsgemäß durch die Merkmale des Anspruchs 1 gelöst. Weitere, besonders vorteilhafte Ausgestaltungen der Erfindung offenbaren die Unteransprüche.This object is achieved by the features of claim 1. Further, particularly advantageous embodiments of the invention disclose the dependent claims.
Die Erfindung beruht im wesentlichen auf dem Gedanken, vor dem Einbringen des Metallpulvers in die Sprengstoffmischung ein Absättigen der polaren Gruppen des Metallpulvers durch SiR3-Gruppen (R = organischer Rest) vorzunehmen. Dadurch können die polaren Gruppen nicht mehr mit den Isocyanaten reagieren und die spezifische Oberfläche des jeweiligen Metallpulvers verringert sich. Ebenso sinkt die Viskosität der Sprengladung. Als organische Reste kommen alle Alkyl- und Arylreste in Betracht, wobei die Alkylreste reaktiver sind.The invention is based essentially on the idea of saturating the polar groups of the metal powder with SiR 3 groups (R = organic radical) before introducing the metal powder into the explosive mixture. As a result, the polar groups can no longer react with the isocyanates and the specific surface area of the respective metal powder decreases. Likewise, the viscosity of the explosive charge decreases. Suitable organic radicals are all alkyl and aryl radicals, the alkyl radicals being more reactive.
Als besonders vorteilhaft hat es sich erwiesen, zur Absättigung der polaren Gruppen des Metallpulvers Trimethylchlorsilan (Me3SiCl) zu verwenden. Dieses reagiert sofort mit den OH-Gruppen und bildet einen Silylether (-O-SiMe3).It has proven particularly advantageous to use trimethylchlorosilane (Me 3 SiCl) to saturate the polar groups of the metal powder. This reacts immediately with the OH groups and forms a silyl ether (-O-SiMe 3 ).
Bei einem Ausführungsbeispiel wurden 100 g Wolframpulver (Korngröße zwischen 3 und 5 µm) in eine Lösung aus 900 g Pentan und 20 g Trimethylchlorsilan eingebracht und 5 Minuten gerührt. Anschließend wurde das Wolframpulver abfiltriert und im Trockenschrank getrocknet. Während die spezifische Oberfläche vor der Behandlung mit Me3SiCl 0,1978 m2/g betrug, betrug sie nach der Behandlung lediglich 0,1880 m2/g, was anschließend zu einer Verringerung der Viskosität der Sprengstoffmischung von ca. 600 - 800 Pas auf ca. 400 Pas führte.In one embodiment, 100 g of tungsten powder (particle size between 3 and 5 microns) were placed in a solution of 900 g of pentane and 20 g of trimethylchlorosilane and stirred for 5 minutes. Subsequently, the tungsten powder was filtered off and dried in a drying oven. While the specific surface before treatment with Me3SiCl was 0.1978 m 2 / g, after treatment it was only 0.1880 m 2 / g, which subsequently led to a reduction of the viscosity of the explosive mixture from approx. 600 - 800 Pas to approx 400 Pas led.
Die Herstellung der erfindungsgemäßen Sprengladungen kann beispielsweise mittels
der nachfolgenden typischen Rezepturen erfolgen:
Dabei sollte die Körngröße des jeweiligen Metallpulvers zwischen 0,1 und 5 µm liegen.The grain size of the respective metal powder should be between 0.1 and 5 μm lie.
Claims (4)
- Method of making pourable, plastic-bound explosive charges or rocket propellants, comprisinga) adding to the explosive charge a metal powder comprising powdered grains with essentially spherical shape and possessing a grain size of between 0.1 to 5 µm andb) before introducing the metal powder into the explosive mixture, saturating the polar groups of the metal powder by reaction with SiR3 groups, in which R is an organic radical.
- Method according to Claim 1, characterized in that the organic radical is an alkyl or aryl radical.
- Method according to Claim 2, characterized in that the polar groups of the metal powder are saturated by reaction with trimethylchlorosilane (Me3SiCl).
- Method according to any one of Claims 1 to 3, characterized in that the metal powder added comprises powders of one or more of the following metals: vanadium, niobium, tantalum, chromium, molybdenum or tungsten.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10107948A DE10107948A1 (en) | 2001-02-20 | 2001-02-20 | Process for the production of pourable plastic-bound explosive charges or rocket fuels |
DE10107948 | 2001-02-20 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1241150A2 EP1241150A2 (en) | 2002-09-18 |
EP1241150A3 EP1241150A3 (en) | 2003-11-05 |
EP1241150B1 true EP1241150B1 (en) | 2005-09-07 |
Family
ID=7674732
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01129902A Expired - Lifetime EP1241150B1 (en) | 2001-02-20 | 2001-12-15 | Process for producing mouldable, plastic-bound explosives or rocket propellants |
Country Status (5)
Country | Link |
---|---|
US (1) | US6558488B2 (en) |
EP (1) | EP1241150B1 (en) |
DE (2) | DE10107948A1 (en) |
IL (1) | IL148248A (en) |
NO (1) | NO321219B1 (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE60221679D1 (en) * | 2001-08-27 | 2007-09-20 | Wiley Organics Inc | ALKYNYLSILANE AS A FUEL AND FUEL FOR ROCKETS |
US8545646B1 (en) * | 2005-06-10 | 2013-10-01 | The United States Of America As Represented By The Secretary Of The Navy | High-density rocket propellant |
US8894739B1 (en) * | 2007-05-23 | 2014-11-25 | The United States Of America As Represented By The Secretary Of The Navy | Metal powders with improved flowability |
US7943084B1 (en) * | 2007-05-23 | 2011-05-17 | The United States Of America As Represented By The Secretary Of The Navy | Metal powders with improved flowability |
DE102010052628A1 (en) | 2010-11-29 | 2012-05-31 | Rheinmetall Waffe Munition Gmbh | Perchlorate-free pyrotechnic mixture |
RU2524500C1 (en) * | 2013-02-05 | 2014-07-27 | Федеральное казенное предприятие "Государственный научно-исследовательский институт химических продуктов" (ФКП "ГосНИИХП") | Fowling 7,62×39-9 cartridge (with 9 g bullet) |
RU2524494C1 (en) * | 2013-03-06 | 2014-07-27 | Федеральное казенное предприятие "Государственный научно-исследовательский институт химических продуктов" (ФКП "ГосНИИХП") | Fowling 7,62×39-10 cartridge (with 9 g bullet) |
Family Cites Families (16)
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US2647047A (en) * | 1950-03-06 | 1953-07-28 | Warren B Richardson | Explosive composition |
USRE27025E (en) * | 1960-02-01 | 1971-01-12 | Mcdonald Louis | Process of conditioning particulate materials with an organosilicon coating for use in organic explosives. |
CA928927A (en) * | 1967-11-14 | 1973-06-26 | Kawakita Takao | Nylon molding article and process for producing the same |
CA1060660A (en) * | 1976-10-28 | 1979-08-21 | Her Majesty The Queen In Right Of Canada As Represented By The Minister Of National Defence Of Her Majesty's Canadian Government | Composite explosives |
US4115165A (en) * | 1977-06-23 | 1978-09-19 | Atlas Powder Company | Hydrophobic aluminum sensitizing agents for explosives |
NO144666C (en) * | 1980-02-29 | 1981-10-14 | Dyno Industrier As | PROCEDURE FOR PREPARING ALUMINUM-CONTAINING HIGH-ENERGY EXPLOSIVE MIXTURES |
DE3234978C1 (en) * | 1982-09-22 | 1984-01-26 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Cast explosive charge |
CA1207588A (en) * | 1983-09-23 | 1986-07-15 | Gordon K. Briosi | Dual-function storage container for prilled explosive |
US4689250A (en) * | 1984-11-16 | 1987-08-25 | Siemens Aktiengesellschaft | Cross-linked polymer coated metal particle filler compositions |
US4696641A (en) * | 1986-08-11 | 1987-09-29 | Gte Products Corporation | Primer material and photoflash lamp |
DE3804396C1 (en) * | 1988-02-12 | 1989-05-18 | Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De | Process for producing plastic-bonded explosives |
US5209976A (en) * | 1988-07-04 | 1993-05-11 | Matsushita Electric Industrial Co., Ltd. | Structure having a surface covered with a monomolecular film |
DE3934368C1 (en) * | 1989-10-14 | 1990-11-15 | Fraunhofer-Gesellschaft Zur Foerderung Der Angewandten Forschung Ev, 8000 Muenchen, De | |
US5547526A (en) * | 1990-03-06 | 1996-08-20 | Daimler-Benz Aerospace Ag | Pressable explosive granular product and pressed explosive charge |
US5123981A (en) * | 1990-06-14 | 1992-06-23 | Atlas Powder Company | Coated solid additives for explosives |
US5451277A (en) * | 1991-05-09 | 1995-09-19 | Aerojet-General Corporation | Preparing solid energetic compositions from coated particles and liquid oxidizers |
-
2001
- 2001-02-20 DE DE10107948A patent/DE10107948A1/en not_active Withdrawn
- 2001-12-15 DE DE50107360T patent/DE50107360D1/en not_active Expired - Lifetime
- 2001-12-15 EP EP01129902A patent/EP1241150B1/en not_active Expired - Lifetime
- 2001-12-20 NO NO20016257A patent/NO321219B1/en not_active IP Right Cessation
-
2002
- 2002-02-19 IL IL148248A patent/IL148248A/en active IP Right Grant
- 2002-02-20 US US10/077,770 patent/US6558488B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
NO321219B1 (en) | 2006-04-03 |
IL148248A0 (en) | 2002-09-12 |
IL148248A (en) | 2007-05-15 |
EP1241150A3 (en) | 2003-11-05 |
DE10107948A1 (en) | 2002-08-22 |
EP1241150A2 (en) | 2002-09-18 |
US20030056865A1 (en) | 2003-03-27 |
US6558488B2 (en) | 2003-05-06 |
NO20016257L (en) | 2002-08-21 |
DE50107360D1 (en) | 2005-10-13 |
NO20016257D0 (en) | 2001-12-20 |
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