USH1459H - High energy explosives - Google Patents

High energy explosives Download PDF

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Publication number
USH1459H
USH1459H US07/233,715 US23371588A USH1459H US H1459 H USH1459 H US H1459H US 23371588 A US23371588 A US 23371588A US H1459 H USH1459 H US H1459H
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explosive
energetic
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US07/233,715
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William G. Lawrence
Robert C. Gill
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US Department of Navy
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US Department of Navy
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Assigned to UNITED STATES OF AMERICA, THE, AS REPRESENTED BY THE SECRETARY OF THE NAVY reassignment UNITED STATES OF AMERICA, THE, AS REPRESENTED BY THE SECRETARY OF THE NAVY ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: GILL, ROBERT C., LAWRENCE, G. WILLIAM
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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
    • C06B45/04Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive
    • C06B45/06Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive the solid solution or matrix containing an organic component
    • C06B45/10Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive the solid solution or matrix containing an organic component the organic component containing a resin
    • C06B45/105The resin being a polymer bearing energetic groups or containing a soluble organic explosive
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G18/00Polymeric products of isocyanates or isothiocyanates
    • C08G18/06Polymeric products of isocyanates or isothiocyanates with compounds having active hydrogen
    • C08G18/28Polymeric products of isocyanates or isothiocyanates with compounds having active hydrogen characterised by the compounds used containing active hydrogen
    • C08G18/30Low-molecular-weight compounds
    • C08G18/38Low-molecular-weight compounds having heteroatoms other than oxygen
    • C08G18/3819Low-molecular-weight compounds having heteroatoms other than oxygen having nitrogen
    • C08G18/384Low-molecular-weight compounds having heteroatoms other than oxygen having nitrogen containing nitro groups
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G18/00Polymeric products of isocyanates or isothiocyanates
    • C08G18/06Polymeric products of isocyanates or isothiocyanates with compounds having active hydrogen
    • C08G18/28Polymeric products of isocyanates or isothiocyanates with compounds having active hydrogen characterised by the compounds used containing active hydrogen
    • C08G18/40High-molecular-weight compounds
    • C08G18/56Polyacetals

Definitions

  • This invention relates to explosives and more particularly to high energy, cast-cured explosives.
  • Another approach is the cast-curing of high energy, non-melt castable explosives in binders of energetic plasticizers, inert polymers, and curatives.
  • the inert polymer substantially reduces the energy density of the resulting explosives.
  • an object of this invention is to provide a new cast-curable explosive.
  • Another object of this invention is to provide a cast-curable explosive having higher energy.
  • a further object of this invention is to provide a means for incorporating non-melt castable explosives into high density, high energy voidless matrices which can be cast-cured.
  • Yet another object of this invention is to provide high energy explosives with safe handling characteristics.
  • R is --CH 2 CF(NO 2 ) 2 or --CH 2 C(NO 2 ) 2 CH 3 ;
  • A is --CH 2 CH 2 , --CH 2 OCH 2 --, or --CH 2 OCH 2 OCH 2 --, and n>1, and
  • energetic plasticizer and explosives are uniformly dispersed throughout the energetic polymer matrix.
  • HMX cyclotetramethylenetetranitramine
  • the cure catalyst and polyisocyanate curing agent are thoroughly mixed into and dispersed uniformly through the prepolymer/plasticizer/explosive mixture. This step is preferably done at a temperature of from 50° to 80° C., or preferably 60° to 65° C.
  • the resulting mixture is cast into suitable devices or molds under vacuum.
  • the molds may be heated or be at room temperature depending on the flow properties of the mixture and the size or intricacy of the mold.
  • the mixture in the mold is then cured with heat at 40° to 60° C. or preferably 48° to 52° C. for about 2 to 7 days.
  • the explosive composite mixture Prior to curing, the explosive composite mixture comprises: (1) the explosive, (2) the energetic prepolymer, (3) the energetic plasticizer, (4) the diisocyanate curing agent, and (5) conventional additive such as a cure catalyst, oxidation inhibitors, etc.
  • the explosive comprises from 50 to 90, preferably from 70 to 85, and more preferably 78.0 to 81.0 weight percent of the uncured explosive composite mixture.
  • the explosive is preferably cyclotetramethylenetetranitramine (HMX), cyclotrimethylenetrinitramine (RDX), 1,3,5-triamino-2,4,6-trinitrobenzene (TATB), 2,2',4,4',6,6'-hexanitrostilbene (HNS), 3-nitro-1,2,4-triazol-5-one (NTO), nitroguanidine (NQ), or mixtures thereof.
  • the energetic prepolymer comprises from 1.487 to 21.59, preferably from 2.70 to 10.00, and more preferably from 4.09 to 6.71 weight percent of the uncured explosive composite mixture.
  • the energetic prepolymers which may be used to form explosive composites of the present invention may be represented by the general formula ##STR4## where R is --CH 2 C(NO 2 ) 2 CH 3 or --CH 2 CF(NO 2 ) 2 and A is --CH 2 CH 2 --, or CH 2 OCH 2 , or --CH 2 OCH 2 OCH 2 --, and wherein n>1.
  • R is --CH 2 C(NO 2 ) 2 CH 3 or --CH 2 CF(NO 2 ) 2
  • A is --CH 2 CH 2 --, or CH 2 OCH 2 , or --CH 2 OCH 2 OCH 2 --, and wherein n>1.
  • These energetic polymers are prepared by reacting diols of the formula
  • the prepolymers used in this invention are of the following formulas ##STR6## which is prepared by reacting bis(2-fluoro-2,2-dinitroethyl)dichloroformal with 2,2,8,8-tetranitro-4,6-dioxanone-1,9-diol; ##STR7## which is prepared by reacting bis(2,2-dinitropropyl)dichlorcformal with 2,2,8,8-tetranitro-4,6-dioxanone-1,9-diol; ##STR8## which can be prepared by reacting bis(2-fluoro-2,2-dinitroethyl)dichloroformal with 2,2,5,5-tetranitrohexane-1,6-diol; ##STR9## which can be prepared by reacting bis(2,2-dinitropropyl)dichloroformal with 2,2,5,5-tetranitrohexane-1,6-diol; ##STR10## which can be prepared
  • equimolar amounts of the diol and the dichloroformal can be used, but preferably an excess of the diol is used to assure that the prepolymer product will be hydroxy-terminated.
  • the molar ratio of diol to the dichloroformal is from 1:1 to 2:1 or preferably from 1.33: 1 to 1.50: 1.
  • the average molecular weight of the hydroxyterminated polynitroorthocarbonate prepolymer is from 1,000 to 10,000.
  • the average molecular weight of the prepolymer produced decreases.
  • the reaction between a diol and the dichloroformal can be run without a solvent by melting the starting materials. However, it is safer and thus preferable to use a solvent.
  • Preferred among the solvents are the chlorohydrocarbons such as methylene chloride, 1,2-dichloroethane, 1,1,1-trichloroethane, 1,1,2-trichloroethane, 1,1,2,2-tetrachloroethane, and choloroform, with chloroform being the preferred solvent.
  • Nitromethane also can be used as the solvent.
  • the reaction temperature is preferably from about 40° C. to about 100° C. and more preferably from 50° C. to 60° C.
  • the reaction temperature is preferably from about 50° C. to about 100° C. and more preferably from 60° C. to 65° C.
  • a rapid stream of dry nitrogen is passed through the reaction mixture to remove hydrogen chloride which is generated by the reaction between the diol and dichloroformal. It is advantageous to collect and titrate the evolved hydrogen chloride to determine and confirm the extent of reaction.
  • the crude polynitroorthocarbonate material is obtained either by solvent evaporation or by decantation of the supernatant liquid from the cooled reaction mixture.
  • Purified material is obtained by extracting the low molecular weight impurities from the crude material with suitable solvents and/or solvent combinations. For example, chloroform or mixture of a few percent ( ⁇ 2%) of methanol in chloroform will work.
  • the starting materials used to prepare the prepolymers may be obtained as follows:
  • the energetic plasticizer comprises from 8.0 to 20.0, preferably from 11.80 to 15.0, and more preferably from 12.50 to 13.10 weight percent of the uncured explosive composite mixture.
  • Preferred energetic plasticizers are bis(2-fluoro-2,2-dinitroethyl)formal (FEFO) , metriol trinitrate (TMETN), nitroglycerin (NG), 1,2,4-butanetriol trinitrate (BTTN), and 2,2,2-trinitroethyl 2-nitroethyl ether (TNEN) .
  • BDNPF bis(2,2-dinitropropyl)formal
  • TEFO bis(2,2,2-trinitroethyl)formal
  • TNEPF 2,2,2-trinitroethyl)-2,2-dinitropropyl)formal
  • A/F bis(2,2-dinitropropyl)acetate and bis(2,2-dinitropropyl)formal
  • the hydroxy-terminated polynitroorthocarbonate prepolymers react with conventional polyisocyanates to produce rubbery polyurethane binders.
  • These polyurethane binders have conventional properties such as strength and flexibility, but they are much more energetic than conventional polyurethane binders.
  • the polyisocyanates comprise from 0.511 to 7.41, preferably from 0.92 to 3.43, and more preferably from 1.41 to 2.29 weight percent of the uncured explosive composite mixture.
  • Conventional polyisocyanates which may be used include aromatic, aliphatic, and cycloaliphatic polyisocyanates such as: 2,4-toluene diisocyanate, 2,6-toluene diisocyanate, p-phenylene diisocyanate, 1,5-naphthylene diisocyanate, 4,4'-biphenylene diisocyanate, p,p'-methylene diphenyl diisocyanate, 1,4-tetramethylene diisocyanate, 1,6-hexamethylene diisocyanate, 1,10-decamethylene diisocyanate, 1,4-cyclohexylene diisocyanate, 4,4'-methylene-bis-cyclohexyl isocyanate), 1,5-tetrahydronaphthy
  • polyisocyanates may also be used.
  • Preferred polyisocyanates are 2,4-toluene diisocyanate, polymethylpolyphenylisocyanate (PAPI), and N,N',N"-trisisocyanatohexylbiuret.
  • PAPI polymethylpolyphenylisocyanate
  • N,N',N"-trisisocyanatohexylbiuret are more preferred.
  • trifunctional isocyanates such as N,N',N"-trisisocyanatohexylbiuret and the T-1890's (Huls Chemische Werke) are more preferred.
  • the T-1890's are polyfunctional oligomers of the cyclic trimer of isophorone diisocyanate. The use of trifunctional alcohols with difunctional isocyanates will also help to reduce void formation.
  • Suitable trifunctional alcohols include 2-nitro-2-(hydroxymethyl)-1,3-propanediol(Nibglcerol), trimethylolpropane (TMP), as well as trifunctional polycaprolactone [e.g., Union Carbide's PCP 310 (mol wt. 900), PCP 301 (mol. wt. 300), PCP 300 (mol wt. 540)].
  • the polyisocyanates are used in an amount sufficient to supply from about 0.8:1 to about 1.5:1 but preferably from 1:1 to 1.2:1 isocyanate functional groups for each hydroxyl functional group.
  • the final cured explosive composite comprises the explosive and a binder which comprises an energetic polyurethane polymer matrix and the energetic plasticizer.
  • the weight percent of explosive in the cured composite is the same as in the uncured composite: from 50 to 90, preferably from 70 to 85, and more preferably from 78.0 to 81.0 based on the total weight of the cured explosive composite.
  • the weight percent of energetic plasticizer in the cured explosive composite is the same as in the uncured composite: from 8.0 to 20.0, preferably from 11.80 to 15.0, and more preferably from 12.50 to 13.10 based on the total weight of the cured explosive composite.
  • the weight of the energetic polyurethane polymer matrix in the cured explosive composite equals the sum of the weights of the (1) energetic prepolymer, (2) the polyisocyanate, and (3) the additives in the uncured explosive composite. Therefore, the weight percent of the energetic polyurethane polymer matrix is from 2 to 30, preferably 4 to 15, and more preferably from 5.90 to 9.50 weight percent based on the total weight of the cured explosive composite.
  • Examples 1 through 18 are summarized in tables 1 (composition of reaction mixture), 2 (physical properties), and 3 (performance data).
  • Example 1, 14, and 17 are first presented in detail to illustrate the method of preparation.
  • HMX B 28.125 g
  • HMX C 42.19 g
  • HMX C 42.19 g
  • aromatic polyfunctional isocyanate PAPI, trade name of the Upjohn Co., 0.354 g
  • TDI toluenediisocyanate
  • TDI 1.052 g
  • HMX B 600 g
  • HMX C 900 g
  • HMX C 900 g
  • 2-nitrodiphenylamine 2NDPA, 6.072 g
  • poly functional oligomers of cyclic trimers of isophoronediisocyanate T-1890s, Huls Chemische Werke, 40.0 g
  • dibutyltin sulfide T-5, M & T Chemicals, 0.03 g
  • HMX B (38.0 g), HMX C (59.85 g), HMX C (59.85 g), and N-methyl-4-nitroaniline (MNA, 0.287 g) and 2-nitrodiphenyl amine (2NDPA, 0.287 g), and polyfunctional oligomers of cyclic trimers of isophoronediisocyanate (T-1890s, Huls Chemische Werke, 3.56 g) and maleic anhydride (MA, 0.574), and triphenylbismuth (Ph 3 Bi, 0.043 g) were added sequentially with 15 minute mixing cycles under vacuum at 60°-65° C. for each addition.
  • PA Picric acid
  • PCP300, PCP301, and PCP310 are available from Union Carbide
  • NC Nitrocellulose (11.87% N, 254 eq. wt.)
  • PAPI Aromatic polyfunctional isocyanate (Upjohn Co.)
  • IPDI Isophorone diisocyanate
  • T-12 Dibutyltin dilaurate
  • Example 19 illustrates the preferred explosive composite (embodiment). It was prepared according to the methods taught in this specification.
  • Examples 20 and 21 illustrate methods by which the bis(2-fluoro-2,2-dinitroethyl)dichloroformal starting material can be prepared. These examples are taken from U.S. patent application Ser. No. 06/256,462 which was filed on Mar. 30, 1981, by William H. Gilligan and which now is under a D-10 order.
  • the bis(2-fluoro-2,2-dinitroethyl)thiocarbonate used in examples 20 and 21 can be prepared according to the method disclosed in example 1 of U.S. Pat. No. 4,172,088, entitled “Bis(2-Fluoro-2,2-dinitroethyl)thionocarbonate and a method of Preparation,” which issued on Oct. 23, 1979, to Angres et al.
  • Example 22 illustrates a method by which the bis(2,2-dinitropropyl)dichloroformal starting material can be prepared. This example is taken from U.S. patent application Ser. No. 06/256,462 which was filed on Mar. 30, 1981, by William H. Gilligan and which now is under a D-10 order.
  • Example 22 The bis(2,2-dinitropropyl)thiocarbonate used in Example 22 is prepared according to a method disclosed in Example 1 of U.S. Pat. No.4,323,518, entitled “Polynitroethylthiocarbonates and Method of Preparation", which issued on Apr. 6, 1982, to William H. Gilligan, herein incorporated by reference.
  • Examples 23 and 24 illustrate the preparation of the prepolymers using bis(2-fluoro-2,2-dinitroethyl)dichloroformal and 2,2,8,8-tetranitro-4,6-dioxanone-1,9-diol as the starting materials. These examples are incorporated from U.S. patent application Ser. No. 06/754,898, filed on May 23, 1985, supra.
  • 2,2,8,8-tetranitro-4,6-dioxanonane-1,9-diol (60.0 g, 0.174 mol), bis(2-fluoro-2,2-dinitroethyl)dichloroformal (54.25 g, 0.139 mol), and ethanol-free chloroform (51.0 mL) were added to a three-necked, round bottomed flask equipped with a nitrogen sparge tube inlet, an insulated, spiral condenser outlet at -25° C., and a motor driven stirrer. A preheated 60°-65° C. oil bath was raised around the flask causing the contents to form a solution quickly.
  • Examples 25 and 26 illustrate the preparation of the prepolymers using bis(2,2-dinitropropyl)dichloroformal and 2,2,8,8-tetranitro-4,6-dioxanane-1,9-diol as starting materials. These examples are incorporated from U.S. patent application Ser. No. 06/754,897 filed on May 23, 1985, supra.
  • the lower layer containing the polymer was extracted four times with 100 ml of chloroform (vide supra). The residual solvent was removed in vacuo and the solid polymer was powdered. Analysis gave the following values: weight average molecular weight, 3870; number average molecular weight, 2621; dispersity, 1.48 and functionality, 1.96.

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Abstract

A high energy explosive composite which comprises
(1) from about 2 to about 30 weight percent of an energetic polymer matrixf a urethane which is the reaction product of
(a) a hydroxy-terminated prepolymer of the formula ##STR1## where R is --CH2 CF(NO2)2 or --CH2 C(NO2)2 CH3 ; A is --CH2 CH2, --CH2 OCH2 --, or --CH2 OCH2 OCH2 --, and n>1, and
(b) a polyisocyanate which is used in an amount sufficient to supply from about 0.8:1 to about 1.5:1 isocyanate functional groups for each hydroxy functional group;
(2) from about 8 to about 20 weight percent of an energetic plasticizer; and
(3) from about 50 to about 90 weight percent of an explosive;
wherein the energetic plasticizer and explosives are uniformly dispersed throughout the energetic polymer matrix.

Description

BACKGROUND OF THE INVENTION
This invention relates to explosives and more particularly to high energy, cast-cured explosives.
At present highly energetic explosives are prepared by melt-casting highly energetic, but non-melt castable, explosives with less energetic, but melt castable explosives. Unfortunately, these high energy, melt-cast explosives have problems in uniformity of casting, in cracking, and in safety characteristics.
Another approach is the cast-curing of high energy, non-melt castable explosives in binders of energetic plasticizers, inert polymers, and curatives. However, the inert polymer substantially reduces the energy density of the resulting explosives.
Thus, it would be desirable to provide cast-curable explosives having higher energy densities.
SUMMARY OF THE INVENTION
Accordingly, an object of this invention is to provide a new cast-curable explosive.
Another object of this invention is to provide a cast-curable explosive having higher energy.
A further object of this invention is to provide a means for incorporating non-melt castable explosives into high density, high energy voidless matrices which can be cast-cured.
Yet another object of this invention is to provide high energy explosives with safe handling characteristics.
These and other objects of this invention are accomplished by providing:
a explosive composite comprising
(1) from about 2 to about 30 weight percent of an energetic polymer matrix of a urethane which is the reaction product of
(a) a hydroxy-terminated prepolymer of the formula ##STR2## where R is --CH2 CF(NO2)2 or --CH2 C(NO2)2 CH3 ; A is --CH2 CH2, --CH2 OCH2 --, or --CH2 OCH2 OCH2 --, and n>1, and
(b) a polyisocyanate which is used in an amount sufficient to supply from about 0.8:1 to about 1.5:1 isocyanate functional groups for each hydroxy functional group;
(2) from about 8 to about 20 weight percent of an energetic plasticizer; and
(3) from about 50 to about 90 weight percent of an explosive;
wherein the energetic plasticizer and explosives are uniformly dispersed throughout the energetic polymer matrix.
DETAILED DESCRIPTION OF THE INVENTION
First, a mixture of an energetic hydroxy-terminated prepolymer of the general formula ##STR3## where R is --CH2 CF(NO2)2 or --CH2 C(NO2)2 CH3, A is --CH2 CH2 --, --CH2 OCH2 --, or --CH2 OCH2 OCH2 --, and n>1 is mixed with an energetic plasticizer and the mixture is dried and degassed. This can be done by heating the mixture for 1-2 hours under vacuum at 65° C. to 70° C.
Next particles of an energetic explosive such as cyclotetramethylenetetranitramine (HMX) are mixed into the prepolymer/plasticizer until the particles are uniformly dispersed throughout the mixture. This mixing operation is preferably done at a temperature of from 50° to 80° C., or more preferably 60° to 65° C.
Next the cure catalyst and polyisocyanate curing agent are thoroughly mixed into and dispersed uniformly through the prepolymer/plasticizer/explosive mixture. This step is preferably done at a temperature of from 50° to 80° C., or preferably 60° to 65° C.
The resulting mixture is cast into suitable devices or molds under vacuum. The molds may be heated or be at room temperature depending on the flow properties of the mixture and the size or intricacy of the mold. The mixture in the mold is then cured with heat at 40° to 60° C. or preferably 48° to 52° C. for about 2 to 7 days.
Prior to curing, the explosive composite mixture comprises: (1) the explosive, (2) the energetic prepolymer, (3) the energetic plasticizer, (4) the diisocyanate curing agent, and (5) conventional additive such as a cure catalyst, oxidation inhibitors, etc.
The explosive comprises from 50 to 90, preferably from 70 to 85, and more preferably 78.0 to 81.0 weight percent of the uncured explosive composite mixture. The explosive is preferably cyclotetramethylenetetranitramine (HMX), cyclotrimethylenetrinitramine (RDX), 1,3,5-triamino-2,4,6-trinitrobenzene (TATB), 2,2',4,4',6,6'-hexanitrostilbene (HNS), 3-nitro-1,2,4-triazol-5-one (NTO), nitroguanidine (NQ), or mixtures thereof.
The energetic prepolymer comprises from 1.487 to 21.59, preferably from 2.70 to 10.00, and more preferably from 4.09 to 6.71 weight percent of the uncured explosive composite mixture.
The energetic prepolymers which may be used to form explosive composites of the present invention may be represented by the general formula ##STR4## where R is --CH2 C(NO2)2 CH3 or --CH2 CF(NO2)2 and A is --CH2 CH2 --, or CH2 OCH2, or --CH2 OCH2 OCH2 --, and wherein n>1. These energetic polymers are prepared by reacting diols of the formula
HOCH.sub.2 C(NO.sub.2).sub.2 --A--C(NO.sub.2).sub.2 CH.sub.2 OH
with dichloroformals of the formula ##STR5## where A and R are as defined above.
Methods of preparing the prepolymers where R is --CH2 CF(NO2)2 are disclosed in U.S. patent application Ser. No. 06/754,898 filed on May 23, 1985, by G. William Lawrence and William H. Gilligan, entitled "Energetic Fluoronitro Prepolymer," (Navy Case No. 68,377), herein incorporated by reference.
Methods of preparing the prepolymer where R is --CH2 C(NO2)2 CH3 are disclosed in U.S. patent application Ser. No. 06/754,897, filed on May 23, 1985, by G. William Lawrence and William H. Gilligan entitled "Energetic Nitro Prepolymer," (Navy Case No. 68,397), herein incorporated by reference.
Specifically, the prepolymers used in this invention are of the following formulas ##STR6## which is prepared by reacting bis(2-fluoro-2,2-dinitroethyl)dichloroformal with 2,2,8,8-tetranitro-4,6-dioxanone-1,9-diol; ##STR7## which is prepared by reacting bis(2,2-dinitropropyl)dichlorcformal with 2,2,8,8-tetranitro-4,6-dioxanone-1,9-diol; ##STR8## which can be prepared by reacting bis(2-fluoro-2,2-dinitroethyl)dichloroformal with 2,2,5,5-tetranitrohexane-1,6-diol; ##STR9## which can be prepared by reacting bis(2,2-dinitropropyl)dichloroformal with 2,2,5,5-tetranitrohexane-1,6-diol; ##STR10## which can be prepared by reacting bis(2-fluoro-2,2-dinitroethyl) dichloroformal with 2,2,6,6-tetranitro-4-oxaheptane-1,7-diol; and ##STR11## which can be prepared by reacting bis(2,2-dinitropropyl)dichloroformal with 2,2,6,6-tetranitro-4-oxaheptane-1,7-diol.
In preparing the polynitroorthocarbonate prepolymers, equimolar amounts of the diol and the dichloroformal can be used, but preferably an excess of the diol is used to assure that the prepolymer product will be hydroxy-terminated. The molar ratio of diol to the dichloroformal is from 1:1 to 2:1 or preferably from 1.33: 1 to 1.50: 1.
Preferably the average molecular weight of the hydroxyterminated polynitroorthocarbonate prepolymer is from 1,000 to 10,000. As the molar ratio of diol to dichloroformal is increased, the average molecular weight of the prepolymer produced decreases.
The reaction between a diol and the dichloroformal can be run without a solvent by melting the starting materials. However, it is safer and thus preferable to use a solvent. Preferred among the solvents are the chlorohydrocarbons such as methylene chloride, 1,2-dichloroethane, 1,1,1-trichloroethane, 1,1,2-trichloroethane, 1,1,2,2-tetrachloroethane, and choloroform, with chloroform being the preferred solvent. Nitromethane also can be used as the solvent.
When bis(2,2-dinitropropyl)dichloroformal is used, the reaction temperature is preferably from about 40° C. to about 100° C. and more preferably from 50° C. to 60° C. However, when bis(2-fluoro-2,2-dinitropropyl)dichloroformal is used, the reaction temperature is preferably from about 50° C. to about 100° C. and more preferably from 60° C. to 65° C.
Preferably a rapid stream of dry nitrogen is passed through the reaction mixture to remove hydrogen chloride which is generated by the reaction between the diol and dichloroformal. It is advantageous to collect and titrate the evolved hydrogen chloride to determine and confirm the extent of reaction.
The crude polynitroorthocarbonate material is obtained either by solvent evaporation or by decantation of the supernatant liquid from the cooled reaction mixture. Purified material is obtained by extracting the low molecular weight impurities from the crude material with suitable solvents and/or solvent combinations. For example, chloroform or mixture of a few percent (˜2%) of methanol in chloroform will work.
The starting materials used to prepare the prepolymers may be obtained as follows:
(1) bis(2-fluoro-2,2-dinitroethyl)dichloroformal can be prepared according to the methods disclosed in examples 20 and 21;
(2) bis(2,2-dinitropropyl)dichloroformal can be prepared according to the method disclosed in example 22;
(3) 2,2,8,8-tetranitro-4,6-dioxanone-1,9-diol, HOCH2 C(NO2)2 CH2 OCH2 OCH2 C(NO2)2 CH2 OH, called DINOL, can be prepared by the method taught at column 4, lines 31-55, of U.S. Pat. No. 3,288,863 titled "Polynitrodiol and Method of Preparation," which issued to Thomas N. Hall and Kathryn G. Shipp on Nov. 29, 1966, herein incorporated by reference;
(4) 2,2,5,5-tetranitrohexane-1,6-diol, HOCH2 C(NO2)2 CH2 CH2 C(NO2)2 CH2 OH, can be prepared according to the method taught in example 1 at column 2, of U.S. Pat. No. 4,374,241 titled "Nitropolyfomals," which issued to Horst G. Adolph on Feb. 15, 1983, herein incorporated by reference; and
(5) 2,2,6,6-tetranitro-4-oxaheptane-1,7-diol, HOCH2 C(NO2)2 CH2 OCH2 C(NO2)2 CH2 OH, can be prepared according to the method taught at column 2, line 59 through column 3, line 10 and also at column 3, lines 31-72 of U.S. Pat. No. 3,531,534 titled "Bisfluorodinitro Ethers and Their Preparation," which issued to Horst G. Adolph on Sep. 29, 1970, herein incorporated by reference.
The energetic plasticizer comprises from 8.0 to 20.0, preferably from 11.80 to 15.0, and more preferably from 12.50 to 13.10 weight percent of the uncured explosive composite mixture. Preferred energetic plasticizers are bis(2-fluoro-2,2-dinitroethyl)formal (FEFO) , metriol trinitrate (TMETN), nitroglycerin (NG), 1,2,4-butanetriol trinitrate (BTTN), and 2,2,2-trinitroethyl 2-nitroethyl ether (TNEN) . Also preferred are mixtures of (1) bis(2, 2-dinitropropyl)formal(BDNPF) , bis(2,2,2-trinitroethyl)formal (TEFO), and (2,2,2-trinitroethyl) (2,2-dinitropropyl)formal (TNEPF), and also (2) bis(2,2-dinitropropyl)acetate and bis(2,2-dinitropropyl)formal (A/F). Other suitable energetic plasticizers may also be used.
The hydroxy-terminated polynitroorthocarbonate prepolymers react with conventional polyisocyanates to produce rubbery polyurethane binders. These polyurethane binders have conventional properties such as strength and flexibility, but they are much more energetic than conventional polyurethane binders.
The polyisocyanates comprise from 0.511 to 7.41, preferably from 0.92 to 3.43, and more preferably from 1.41 to 2.29 weight percent of the uncured explosive composite mixture. Conventional polyisocyanates which may be used include aromatic, aliphatic, and cycloaliphatic polyisocyanates such as: 2,4-toluene diisocyanate, 2,6-toluene diisocyanate, p-phenylene diisocyanate, 1,5-naphthylene diisocyanate, 4,4'-biphenylene diisocyanate, p,p'-methylene diphenyl diisocyanate, 1,4-tetramethylene diisocyanate, 1,6-hexamethylene diisocyanate, 1,10-decamethylene diisocyanate, 1,4-cyclohexylene diisocyanate, 4,4'-methylene-bis-cyclohexyl isocyanate), 1,5-tetrahydronaphthylene diisocyanate, and polymethylenepolyphenylisocyanate (PAPI), isophorone diisocyanate, and N,N',N"-trisisocyanatohexylbiuret. Mixture of polyisocyanates may also be used. Preferred polyisocyanates are 2,4-toluene diisocyanate, polymethylpolyphenylisocyanate (PAPI), and N,N',N"-trisisocyanatohexylbiuret. In order to minimize void formation, trifunctional isocyanates such as N,N',N"-trisisocyanatohexylbiuret and the T-1890's (Huls Chemische Werke) are more preferred. The T-1890's are polyfunctional oligomers of the cyclic trimer of isophorone diisocyanate. The use of trifunctional alcohols with difunctional isocyanates will also help to reduce void formation. Suitable trifunctional alcohols include 2-nitro-2-(hydroxymethyl)-1,3-propanediol(Nibglcerol), trimethylolpropane (TMP), as well as trifunctional polycaprolactone [e.g., Union Carbide's PCP 310 (mol wt. 900), PCP 301 (mol. wt. 300), PCP 300 (mol wt. 540)]. The polyisocyanates are used in an amount sufficient to supply from about 0.8:1 to about 1.5:1 but preferably from 1:1 to 1.2:1 isocyanate functional groups for each hydroxyl functional group.
The final cured explosive composite comprises the explosive and a binder which comprises an energetic polyurethane polymer matrix and the energetic plasticizer. The weight percent of explosive in the cured composite is the same as in the uncured composite: from 50 to 90, preferably from 70 to 85, and more preferably from 78.0 to 81.0 based on the total weight of the cured explosive composite. Similarly, the weight percent of energetic plasticizer in the cured explosive composite is the same as in the uncured composite: from 8.0 to 20.0, preferably from 11.80 to 15.0, and more preferably from 12.50 to 13.10 based on the total weight of the cured explosive composite. However, the weight of the energetic polyurethane polymer matrix in the cured explosive composite equals the sum of the weights of the (1) energetic prepolymer, (2) the polyisocyanate, and (3) the additives in the uncured explosive composite. Therefore, the weight percent of the energetic polyurethane polymer matrix is from 2 to 30, preferably 4 to 15, and more preferably from 5.90 to 9.50 weight percent based on the total weight of the cured explosive composite.
The general nature of the invention having been set forth, the following examples are presented as specific illustrations thereof. It will be understood that the invention is not limited to these examples but is susceptable to various modifications that will be recognized by one of ordinary skill in the art.
Examples 1 through 18 are summarized in tables 1 (composition of reaction mixture), 2 (physical properties), and 3 (performance data).
Example 1, 14, and 17 are first presented in detail to illustrate the method of preparation.
EXAMPLE 1
Bis(2-fluoro-2,2-dinitroethyl)formal (FEFO, 21.086 g), picric acid (1.102 g), and dibutyltin dilaurate (0.149 g) were stirred at 55° C. under vacuum overnight to dry and degas the solution. Prepolymer I (R=--CH2 CF(NO2)2, A=--CH2 OCH2 OCH2 --, 14.80 g, 1033.5 g/equivalent hydroxyl ) was added. After 3 hours at 55° C. under vacuum, this solution was transferred to a high shear mixer (half pint Baker-Perkin) . HMX B (28.125 g), HMX C (42.19 g), HMX C (42.19 g), and aromatic polyfunctional isocyanate (PAPI, trade name of the Upjohn Co., 0.354 g) and toluenediisocyanate (TDI, 1.052 g) were added sequentially with 15 minute mixing cycles under vacuum at 55° C. for each addition. The mixture was vacuum cast into standard JANNAF physical test specimen molds and heated at 55° C. for 4 days. On removing the specimens the material was soft and sticky with a few voids. For composition and physical properties see example No. 1, Tables 1 and 2, respectively.
EXAMPLE 14
Bis(2-fluoro-2,2-dinitroethyl)formal (FEFO 384.74 g) and prepolymer II (R=--CH2 C(NO2)2 CH3, A=--CH2 OCH2 OCH2 --, 174.29 g, 1479 g/equivalent hydroxyl) were stirred in a high shear mixer (one gallon Baker-Perkin) at 65°-70° C. for 2 hours under vacuum to degas and dry the solution. HMX B (600 g), HMX C (900 g), HMX C (900 g), and 2-nitrodiphenylamine (2NDPA, 6.072 g), and poly functional oligomers of cyclic trimers of isophoronediisocyanate (T-1890s, Huls Chemische Werke, 40.0 g) and dibutyltin sulfide (T-5, M & T Chemicals, 0.03 g) were added sequentially with 15 minute mixing cycles under vacuum at 60°-65° C. for each addition. The mixture was vacuum cast into tubes and heated at 48°-52° C. for 12 days. On x-raying the samples, no voids, cracks, or bubbles were found. See Example No. 14, Tables 1, 2, and 3 for composition, physical properties, and performance data respectively.
EXAMPLE 17
bis(2-fluoro-2,2-dinitroethyl)formal (FEFO, 16.86 g), metriol trinitrate (TMETN, 2.95 g), and prepolymer II (R=--CH2 C(NO2)2 CH3, A=--CH2 OCH2 OCH2 --, 8.83 g, 885 g/equivalent hydroxyl) were stirred in a high shear mixer (half pint Baker-Perkin) at 65°-70° C. for 1.5 hours under vacuum. HMX B (38.0 g), HMX C (59.85 g), HMX C (59.85 g), and N-methyl-4-nitroaniline (MNA, 0.287 g) and 2-nitrodiphenyl amine (2NDPA, 0.287 g), and polyfunctional oligomers of cyclic trimers of isophoronediisocyanate (T-1890s, Huls Chemische Werke, 3.56 g) and maleic anhydride (MA, 0.574), and triphenylbismuth (Ph3 Bi, 0.043 g) were added sequentially with 15 minute mixing cycles under vacuum at 60°-65° C. for each addition. The mixture was vacuum cast into standard JANNAF tensile specimens and cured at 48°-52° C. for 7 days. On removing the specimens from the molds the material was found to be fairly strong, not sticky, with no obvious voids. For composition and physical property data see Example No. 17, tables 1 & 2, respectively.
The following glossary defines the abbreviations used in Table 1.
NOMENCLATURE Plasticizers
FEFO=Bis(2-fluoro-2,2-dinitroethyl)formal
TMETN=Metriol trinitrate
Additives
PA=Picric acid
TMP=Trimethylolpropane
EG=Ethyleneglycol
DEG=Diethyleneglycol
PCP310+Trifunctional polycaprolactone (mol. wk.=900)
PCP301=Trifunctional polycaprolactone (mol. wt.=300)
PCP300=Trifunctional polycaprolactone (mol. wt.=540)
(Note: PCP300, PCP301, and PCP310 are available from Union Carbide)
TP=N-Phenyltoluenesulfonamide
2NDPA=2-Nitrodiphenylamine
MNA=N-Methyl-p-nitroaniline
DHE=Bis(hydroxyethyl)hydantoin
NC=Nitrocellulose (11.87% N, 254 eq. wt.)
Isocyanates
TDI=Toluenediisocyanate
PAPI=Aromatic polyfunctional isocyanate (Upjohn Co.)
IPDI=Isophorone diisocyanate
T-1890s--Polyfunctional oligomers of the cyclic trimer of IPDI
Catalysts
T-12=Dibutyltin dilaurate
T-5--Dibutyltin sulfide
ZnOct.=Zinc Octoate
Ph3 Bi=Triphenylbismuth
FEAA=Ferric acetylacetonate
MA=Maleic anhydride
Example 19 illustrates the preferred explosive composite (embodiment). It was prepared according to the methods taught in this specification.
                                  TABLE 1                                 
__________________________________________________________________________
EXPLOSIVE COMPOSITION BY WEIGHT PERCENT                                   
EXAMPLE                                                                   
       PREPOLYMER.sup.(1)                                                 
                 PLASTICIZER.sup.(2)                                      
No.    (EW)      (FEFO)   ADDITIVES                                       
                                   ISOCYANATES                            
                                            CATALYST HMX                  
                                                          HMX             
__________________________________________________________________________
                                                          B               
1      9.78      13.45    0.733    0.705/0.256                            
                                            0.098    56.25                
                                                          18.75           
       (1034)             (PA)     (TDI/PAPI)                             
                                            (T-12)                        
2      7.44      13.06    0.258    1.056    0.018    58.62                
                                                          19.54           
       (1290)             (TMP)    (TDI)    (T-12)                        
3      6.84      11.97    0.159/0.0538                                    
                                   0.962    0.0118   60.00                
                                                          20.00           
       (1329)             (TMP/EG) (TDI)    (ZnOct.)                      
4      5.969     12.93    0.102/0.119                                     
                                   0.840    0.0197/0.204                  
                                                     69.997               
                                                          9.998           
       (1329)             (TMP/DEG)                                       
                                   (TDI)    (ZnOct./Ph.sub.3 Bi)          
5      5.998     13.00    0.046/0.111                                     
                                   0.750    0.0281/0.090                  
                                                     55.99                
                                                          23.99           
       (1892)             (TMP/DEG)                                       
                                   (IPDI)   (FEAA/T-5)                    
6      5.958     12.91    0.067/0.159                                     
                                   0.835    0.0118   60.20                
                                                          19.86           
       (1329)             (TMP/DEG)                                       
                                   (TDI)    (T-5)                         
7      5.956     12.91    0.0668/0.159                                    
                                   0.835    0.019/0.019                   
                                                     60.18                
                                                          19.85           
       (1329)             (TMP/DEG)                                       
                                   (TDI)    (ZnOct/Ph.sub.3 Bi)           
8      5.93      12.86    0.0744/0.197                                    
                                   0.832    0.0198/0.0396                 
                                                     60.27                
                                                          19.78           
       (1329)             (PCP301/DEG)                                    
                                   (TDI)    (ZnOct./Ph.sub.3 Bi)          
9      6.04      12.89    0.043/0.152/0.051                               
                                   0.719    0.099/0.639                   
                                                     60.03                
                                                          20.01           
       (1584)             (TMP/DEG/TP)                                    
                                   (TDI)    (ZnOct./Ph.sub.3 Bi)          
10     5.99      13.11    --       0.720/1.422                            
                                            0.0532   60.00                
                                                          20.00           
       (1892)                      (IPDI/T-1890s)                         
                                            (T-5)                         
11     5.68      12.54    0.195    0.000/1.58                             
                                            0.0093   60.00                
                                                          20.00           
       (1253)             (2NDPA)  (IPDI/T-1890s)                         
                                            (T-5)                         
12     5.66      12.76    0.202    0.000/1.38                             
                                            0.00275  60.00                
                                                          20.00           
       (1476)             (2NDPA)  (IPDI/T-1890s)                         
                                            (T-5)                         
13     5.82      12.74    0.200    0.163/0.933                            
                                            0.00150  60.00                
                                                          20.00           
       (1476)             (2NDPA)  (IPDI/T-1890s)                         
                                            (T-5)                         
14     5.68      12.54    0.194    0.00/1.58                              
                                            0.0093   60.00                
                                                          20.00           
       (1476)             (2NDPA)  (IPDI/T-1890s)                         
                                            (T-5)                         
15     5.98      13.20    0.200    0.598    0.0040   60.00                
                                                          20.00           
       (1365)             (CaSO.sub.4)                                    
                                   (PAPI 94)                              
                                            (T-5)                         
16     5.36      12.15    0.177/0.377                                     
                                   0.254/1.68                             
                                            0.0178   60.00                
                                                          20.00           
       (1500)             (2NDPA/DHE)                                     
                                   (IPDI/T-1890s)                         
                                            (T-5)                         
17     4.525     9.31/1.04                                                
                          0.234/0.0301                                    
                                   0.00/1.827                             
                                            0.0757/0.0302                 
                                                     62.95                
                                                          19.98           
       (885)     (FEFO/TMETN)                                             
                          (MNA/NC) (IPDI/T-1890s)                         
                                            (MA/Ph.sub.3 Bi)              
18     4.526     8.69/1.55                                                
                          0.151/0.151                                     
                                   0.00/1.874                             
                                            0.0302/0.0226                 
                                                     63.00                
                                                          20.00           
       (885)     (FEFO/TMETN)                                             
                          (MNA/2NDPA)                                     
                                   (IPDI/T-1890s)                         
                                            (MA/Ph.sub.3 Bi)              
__________________________________________________________________________
 .sup.(1) Prepolymer I (R = --CH.sub.2 CF(NO.sub.2).sub.2, A =  --CH.sub.2
 OCH.sub.2 OCH.sub.2) was used in example 1. Prepolymer II (R = --CH.sub.2
 C(NO.sub.2).sub.2 CH.sub.3, A = CH.sub.2 OCH.sub.2 OCH.sub.2) was used in
 the remaining examples 2 through 18. The hydroxyl equivalent weights (EW)
 are given in parenthesis beneath the weight percentages.                 
 .sup.(2) Plasticizer used in examples 1 through 16 was                   
 bis(2fluoro-2,2-dinitroethyl)formal (FEFO). in examples 17 and 18 a      
 mixture of FEFO and metriol trinitrate (TMETN) was used as the           
 plasticizer.                                                             
                                  TABLE 2                                 
__________________________________________________________________________
PHYSICAL PROPERTIES OF CAST EXPLOSIVES                                    
   Viscosity                                                              
          Pot Life                                                        
                  Density                                                 
                       S.sub.m.sup.(1)                                    
                          E.sub.m.sup.(2)                                 
                                W.sup.(4)                                 
                                    Shore A                               
No.                                                                       
   (EOM, KP)                                                              
          (HRS to 20 KP)                                                  
                  (g/mL)                                                  
                       (psi)                                              
                          (%)                                             
                             Y.sup.(3)                                    
                                (ft-lb)                                   
                                    Hardness                              
__________________________________________________________________________
1  --     --      1.795                                                   
                       13.0                                               
                          41.3                                            
                              52                                          
                                0.372                                     
                                    11                                    
2  13.3   0.67    1.748                                                   
                       83.0                                               
                          7.26                                            
                             1520                                         
                                0.304                                     
                                    77                                    
3  25     0       1.773                                                   
                       102.0                                              
                          10.15                                           
                             1379                                         
                                0.519                                     
                                    78                                    
4  25     0       1.770                                                   
                       86.                                                
                          7.74                                            
                             1512                                         
                                0.321                                     
                                    72                                    
5  30     0            NO Cure                                            
6  19.8   --      1.750                                                   
                       66 6.78                                            
                             1215                                         
                                0.223                                     
                                    74                                    
7  19.2   --      1.710                                                   
                       48 8.79                                            
                              800                                         
                                0.228                                     
                                    66                                    
8  12.0   --      1.480                                                   
                       26 9.46                                            
                              359                                         
                                0.131                                     
                                    40                                    
9  9.4    1.5     1.580                                                   
                       25 10.86                                           
                              352                                         
                                0.158                                     
                                    31                                    
10 32     0       1.748                                                   
                       Poor Casting 50                                    
11 6      --      1.813                                                   
                       47 4.63                                            
                             1268                                         
                                 0.0412                                   
                                    70                                    
12 8      2.5     1.822                                                   
                       62 4.63                                            
                             1681                                         
                                 0.0608                                   
                                    75                                    
13 18.8   --      1.814                                                   
                       43 5.56                                            
                              583                                         
                                 0.0675                                   
                                    62                                    
14 7.3    3.5     1.812                                                   
                       -- -- -- --  35                                    
15 11.9   --      1.815                                                   
                       43 10.2                                            
                              569                                         
                                0.123                                     
                                    50                                    
16 15.1   --           93 6.48                                            
                             1690                                         
                                0.100                                     
                                    85                                    
17 24.3   0            67 7.87                                            
                             1252                                         
18 13.28                                                                  
__________________________________________________________________________
 .sup.(1) S.sub.m = Maximum stress                                        
 .sup.(2) E.sub.m = Elongation at maximum stress                          
 .sup.(3) Y = Modulus                                                     
 .sup.(4) W = Area under stressstrain curve                               
                                  TABLE 3                                 
__________________________________________________________________________
PERFORMANCE DATA FOR CAST EXPLOSIVES                                      
   Vacuum Thermal                                                         
            Impact Sen.                                                   
                   Large Scale                                            
                          Detonation                                      
   Stability                                                              
            50% Height                                                    
                   Gap Test                                               
                          Velocity                                        
                                Growth   Exudation                        
No.                                                                       
   (48 hrs, cc/g)                                                         
            (cm)   (cards)                                                
                          (mm/sec)                                        
                                (% vol. Change)                           
                                         (%)                              
__________________________________________________________________________
2  0.83     31.7   --     --    --       --                               
9  --       --     --     --    -2.02    0                                
11 0.92     --     --     --    --       --                               
12 0.94     --     --     --    --       --                               
14 --       --     177    8.545 -0.46    0.28                             
15 1.15     --     --     0     --       --                               
__________________________________________________________________________
EXAMPLE 19
______________________________________                                    
                               Percent By                                 
Component.sup.1 Function       Weight                                     
______________________________________                                    
HMX Grade B, Class 3                                                      
                High Explosive 60.00                                      
HMX Grade B, Class 2                                                      
                High Explosive 20.00                                      
Gilligan Prepolymer No. II                                                
                Energetic prepolymer                                      
                               4.88                                       
Bis(2,2,2-fluorodinitro-                                                  
                Energetic plasticizer                                     
                               13.042                                     
ethel formal (FEFO)                                                       
IPDI-T1890s     Crosslinking Agent                                        
                               1.675                                      
(polyisocyanate of                                                        
isophorone diisocyanate)                                                  
2-nitrodiphenylamine                                                      
                Stabilizer     0.164                                      
N-Methyl-4-nitroaniline                                                   
                Stabilizer     0.164                                      
Maleic anhydride                                                          
                Cure agent     0.049                                      
Triphenylbismuth                                                          
                Cure catalyst  0.025                                      
______________________________________                                    
 .sup.1 Gilligan prepolymer II (R = --CH.sub.2 C(NO.sub.2).sub.2 CH.sub.3,
 A = --CH.sub.2 OCH.sub.2 OCH.sub.2 --, 1479 g/equivalent hydroxyl) see   
 formula (II) on page 7.                                                  
Examples 20 and 21 illustrate methods by which the bis(2-fluoro-2,2-dinitroethyl)dichloroformal starting material can be prepared. These examples are taken from U.S. patent application Ser. No. 06/256,462 which was filed on Mar. 30, 1981, by William H. Gilligan and which now is under a D-10 order.
EXAMPLE 20 Bis(2-fluoro- 2,2-dinitroethyl)dichloroformal (Prior Art)
To a solution of 10.0 g (28.6 mmol) of bis(2-fluoro-2,2-dinitroethyl) thionocarbonate in 50 ml of freshly distilled sulfuryl chloride was added 4.0 ml of titanium tetrachloride. The solution was then refluxed for 5 days. Excess sulfuryl chloride and titanium tetrachloride were then removed in vacuo at a bath temperature of 50° C. The solid residue was recrystallized from chloroform to give 7.91 g (71%) of bis(2-fluoro-2,2-dinitroethyl)dichloroformal as colorless crystals, mp 57°-58° C.
H - NMR (CDCl3 /TMS) δ (ppm) - d, 5.02.
Calc. for C5 H4 Cl2 F2 N4 O10 : C, 15.44; H, 1.04; Cl, 18.23; F, 9.77; N, 14.40 Found: C, 15.46; H, 1.05; C1, 18.40; F, 9.98; N, 14.11.
EXAMPLE 21 Bis(2- fluoro-2,2-dinitroethyl)dichloroformal (Prior Art)
Gaseous chlorine was slowly passed into a stirred slurry of 21.0 g (0.067 mol) of bis(2-fluoro-2,2-dinitroethyl)thionocarbonate in 100 ml of dry carbon tetrachloride and 10 ml of dry trifluoroethanol for 4.5 hours at the end of this period the slurry had changed into a clear orange-colored solution. After standing overnight, volatiles were removed on a Rotovac and the solid residue was recrystallized from chloroform to give 19.33 g (83%) of bis(2-fluoro-2,2-dinitroethyl)dichloroformal, m.p. 57°-8° C.
The bis(2-fluoro-2,2-dinitroethyl)thiocarbonate used in examples 20 and 21 can be prepared according to the method disclosed in example 1 of U.S. Pat. No. 4,172,088, entitled "Bis(2-Fluoro-2,2-dinitroethyl)thionocarbonate and a method of Preparation," which issued on Oct. 23, 1979, to Angres et al.
Example 22 illustrates a method by which the bis(2,2-dinitropropyl)dichloroformal starting material can be prepared. This example is taken from U.S. patent application Ser. No. 06/256,462 which was filed on Mar. 30, 1981, by William H. Gilligan and which now is under a D-10 order.
EXAMPLE 22 Bis(2,2-dinitropropyl)dichloroformal (Prior Art)
Gaseous chlorine was passed into a solution of 3.1 g (9.1 mmol) of bis(2,2-dinitropropyl)thionocarbonate in 7 ml of acetonitrile/1,2-dichloroethane mixture (3/4; v/v) for 51/2 hours. After standing overnight, the solvents were removed and the solid residue recrystallized from 1,2-dichloroethane to give 3.2 g (93%) of product, m.p. 121°-3° C.
H - NMR (acetone-Cl6 /TMS) δ (ppm) - s, 5.04; s, 2.39
Calc for C7 H10 N4 O10 Cl2. C, 22.06; H, 2.65; C1, 18.61. Found: C, 22.30; H, 2.68; Cl, 18.28.
The bis(2,2-dinitropropyl)thiocarbonate used in Example 22 is prepared according to a method disclosed in Example 1 of U.S. Pat. No.4,323,518, entitled "Polynitroethylthiocarbonates and Method of Preparation", which issued on Apr. 6, 1982, to William H. Gilligan, herein incorporated by reference.
Examples 23 and 24 illustrate the preparation of the prepolymers using bis(2-fluoro-2,2-dinitroethyl)dichloroformal and 2,2,8,8-tetranitro-4,6-dioxanone-1,9-diol as the starting materials. These examples are incorporated from U.S. patent application Ser. No. 06/754,898, filed on May 23, 1985, supra.
EXAMPLE 23 prior art
To a three-necked, round bottomed flask equipped with a nitrogen inlet, a motor driven stirrer, and an insulated spiral condenser outlet which was cooled at -30° C. were added 2,2,8,8-tetranitro-4,6-dioxanonane-1,9-diol (DINOL, 20.0 g, 0. 0581 mol ), bis(2-fluoro-2,2-dinitroethyl)dichloroformal (19.31 g, 0.0496 mol) and 1,2-dichloroethane (13.0 mL). A preheated 75° C. oil bath was raised around the flask causing the contents to form a solution quickly. A rapid, steady stream of nitrogen was passed through the solution via a sintered glass sparge tube throughout the course of the reaction. After six days, 98.24% of the calculated amount of hydrogen chloride had been trapped by an aqueous sodium hydroxide solution (0.1N). A white solid was isolated by evaporation of the solvent under vacuum and allowing the foam thus formed to solidify. The hydroxyl equivalent weight corrected for the extent of reaction was 1785, measured from the decrease in the infrared absorption of toluenesulfonylisocyanate. The number average molecular weight calculated from the reactant ratio corrected for the extent of reaction was 3792. Thus, the functionality was 2.12.
EXAMPLE 24
2,2,8,8-tetranitro-4,6-dioxanonane-1,9-diol (60.0 g, 0.174 mol), bis(2-fluoro-2,2-dinitroethyl)dichloroformal (54.25 g, 0.139 mol), and ethanol-free chloroform (51.0 mL) were added to a three-necked, round bottomed flask equipped with a nitrogen sparge tube inlet, an insulated, spiral condenser outlet at -25° C., and a motor driven stirrer. A preheated 60°-65° C. oil bath was raised around the flask causing the contents to form a solution quickly. A rapid, steady stream of nitrogen was passed through the solution throughout the course of the reaction. After 25 hours, 81% of the calculated amount of hydrogen chloride had been trapped in an aqueous sodium hydroxide (0.1N) solution. The supernatant liquid was decanted from the cooled mixture. The residue in the flask was extracted with stirring two times with 2% methanol-chloroform and two times with 100% chloroform. The remaining solvent was removed in vacuo, and the solid foam was powdered.
Yield: 69.85 g (66.93% overall yield, 95.92% based on the extent of reaction). The hydroxyl equivalent weight of the material, corrected for the presence of some (˜5-8%) nonfunctional cyclic orthocarbonate, was 998.3 g/eq. OH. Analysis by gel permeation chromatography gave the following corrected values: weight average molecular weight of 2830, number average molecular weight of 2121, and dispersity of 1.33. Thus, the average functionality of the chains above 1000 molecular weight is 2.12.
Examples 25 and 26 illustrate the preparation of the prepolymers using bis(2,2-dinitropropyl)dichloroformal and 2,2,8,8-tetranitro-4,6-dioxanane-1,9-diol as starting materials. These examples are incorporated from U.S. patent application Ser. No. 06/754,897 filed on May 23, 1985, supra.
EXAMPLE 25 (prior art)
To a flask equipped with a nitrogen inlet, a motor-driven stirrer and an insulated spiral condenser at -30° C. was added 76 ml of ethanol-free chloroform. After placing the flask in a 55° C. oil bath, 41.15 g (0.108 mol) of bis(2,2-dinitropropyl)dichloroformal and 43.36 g (0.126 mol) of 2,2,8,8-tetranitro-4,6-dioxanonane-1,9-diol were added. A steady stream of nitrogen was passed through the solution during the course of the reaction. After 5 hours at 55° C., 100.3% of the theoretical amount of hydrogen chloride had been collected. The reaction mixture was then cooled and the upper layer of chloroform was removed by decantation. The bottom layer containing the polymer was washed four times with 70 ml of chloroform by heating to 55° C. for several hours with efficient stirring, then cooling the mixture and removing the chloroform by decantation. After washing, the residual solvent was removed in vacuo to give, after grinding a white powder. Analysis by gel permeation chromatography gave the following values: weight average molecular weight, 4477; number average molecular weight, 2896; dispersity, 1.55 and functionality, 1.99.
EXAMPLE 26 (prior art)
b 2,2,8,8-tetranitro-4,6-dioxanonane-1,9-diol (103.2 g, 0.30 mol) was dissolved in 190 ml ethanol-free chloroform at 55° C. in a resin flask equipped with a nitrogen inlet, a motor-driven stirrer and an insulated spiral condenser at -35°. Then 91.50 g (0.24 mol) of bis(2,2-dinitropropyl)dichloroformal was added and the stirred reaction mixture was held at 55° C. for 7 hours while a steady stream of nitrogen was passed through the mixture. The reaction mixture was cooled and the upper layer of chloroform was removed by decantation. The lower layer containing the polymer was extracted four times with 100 ml of chloroform (vide supra). The residual solvent was removed in vacuo and the solid polymer was powdered. Analysis gave the following values: weight average molecular weight, 3870; number average molecular weight, 2621; dispersity, 1.48 and functionality, 1.96.
Obviously, many modifications and variations of the present invention are possible in light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.

Claims (11)

We claim:
1. An explosive composite comprising:
(1) from about 2 to about 30 weight percent of an energetic polymer matrix of a urethane which is the reaction product of
(a) a hydroxy-terminated prepolymer of the formula ##STR12## where R is selected from the group consisting of --CH2 CF(NO2)2 and --CH2 C(NO2)2 CH3 --, and A is selected from the group consisting of --CH2 CH2, --CH2 OCH2 --, and --CH2 OCH2 OCH2 --, and n>1, and
(b) a polyisocyanate which is used in an amount sufficient to supply from about 0.8:1 to about 1.5:1 isocyanate functional groups for each hydroxy functional group;
(2) from about 8 to about 20 weight percent of an energetic plasticizer; and
(3) from about 50 to about 90 weight percent of an explosive;
wherein the energetic plasticizer and explosive are uniformly dispersed throughout the energetic polymer matrix.
2. The explosive composite of claim 1 wherein R is --CH2 CF(NO2)2.
3. The explosive composite of claim 1 wherein R is --CH2 C (NO2)2 CH3.
4. The explosive composite of claim 1 wherein A is --CH2 CH2 --.
5. The explosive composite of claim 1 wherein A is --CH2 OCH2 --.
6. The explosive composite of claim 1 wherein A is --CH2 OCH2 OCH2 --.
7. The explosive composite of claim 1 comprising (a) from 4 to 15 weight percent of energetic polymer matrix, (b) from 11.8 to 15.0 weight percent of energetic plasticizer, and (c) from 70 to 85 weight percent of explosive.
8. The explosive composite of claim 7 comprising (a) from 5.90 to 9.50 weight percent of energetic polymer matrix, (b) from 12.50 to 13.10 weight percent of energetic plasticizer, (c) and from 78.0 to 81.0 weight percent of explosive.
9. The explosive composite of claim 1 wherein the energetic plasticizer is selected from the group consisting of bis(2-fluoro-2,2-dinitroethyl)formal, metriol trinitrate, nitroglycerin, 1,2,4-butanetriol trinitrate, 2,2,2-trinitroethyl 2-nitroethyl ether, and a binary mixture of bis(2,2-dinitropropyl)formal and bis(2,2-dinitropropyl)acetate.
10. The explosive composite of claim 9 wherein the energetic plasticizer is bis(2-fluoro-2,2-dinitroethyl)formal.
11. The explosive composite of claim 1 wherein the explosive is selected from the group consisting of cyclotetramethylenetetranitramine, cyclotrimethylenetrinitramine, 1,3,5-triamino-2,4,6-trinitrobenzene, 2,2',4,4',6,6'-hexanitrostilbene, 3-nitro-1,2,4-triazol-5-one, nitroguanidine, and mixtures thereof.
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5834685A (en) * 1995-05-10 1998-11-10 Nof Corporation Gas generator composition with azidomethyl group and iron compound modifier

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5834685A (en) * 1995-05-10 1998-11-10 Nof Corporation Gas generator composition with azidomethyl group and iron compound modifier

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