US3907907A - 2-Fluoro-2,2-dinitroethyl substituted polyethers - Google Patents

2-Fluoro-2,2-dinitroethyl substituted polyethers Download PDF

Info

Publication number
US3907907A
US3907907A US729822A US72982268A US3907907A US 3907907 A US3907907 A US 3907907A US 729822 A US729822 A US 729822A US 72982268 A US72982268 A US 72982268A US 3907907 A US3907907 A US 3907907A
Authority
US
United States
Prior art keywords
explosive
reaction
energetic
dinitroethyl
methylene chloride
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
Application number
US729822A
Inventor
Milton B Frankel
Edward F Witucki
David N Vincent
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing North American Inc
Original Assignee
Rockwell International Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rockwell International Corp filed Critical Rockwell International Corp
Priority to US729822A priority Critical patent/US3907907A/en
Application granted granted Critical
Publication of US3907907A publication Critical patent/US3907907A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C07ORGANIC CHEMISTRY
    • C07DHETEROCYCLIC COMPOUNDS
    • C07D303/00Compounds containing three-membered rings having one oxygen atom as the only ring hetero atom
    • C07D303/02Compounds containing oxirane rings
    • C07D303/12Compounds containing oxirane rings with hydrocarbon radicals, substituted by singly or doubly bound oxygen atoms
    • C07D303/18Compounds containing oxirane rings with hydrocarbon radicals, substituted by singly or doubly bound oxygen atoms by etherified hydroxyl radicals
    • C07D303/20Ethers with hydroxy compounds containing no oxirane rings
    • C07D303/22Ethers with hydroxy compounds containing no oxirane rings with monohydroxy compounds
    • 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
    • C08G65/00Macromolecular compounds obtained by reactions forming an ether link in the main chain of the macromolecule
    • C08G65/02Macromolecular compounds obtained by reactions forming an ether link in the main chain of the macromolecule from cyclic ethers by opening of the heterocyclic ring
    • C08G65/04Macromolecular compounds obtained by reactions forming an ether link in the main chain of the macromolecule from cyclic ethers by opening of the heterocyclic ring from cyclic ethers only
    • C08G65/22Cyclic ethers having at least one atom other than carbon and hydrogen outside the ring
    • C08G65/223Cyclic ethers having at least one atom other than carbon and hydrogen outside the ring containing halogens
    • C08G65/226Cyclic ethers having at least one atom other than carbon and hydrogen outside the ring containing halogens containing fluorine

Definitions

  • ABSTRACT This invention is concerned with novel, energetic monomeric epoxy aliphatic ethers terminated with a dinitrofluoro moiety and with the polymers prepared therefrom.
  • the monomers are of the general formula and the polymers are of the general formula wherein R is a lower alkylene of l to 4 carbon atoms, and wherein n is a positive number of from 4 to 25.
  • Chemical explosives and propellants of the aliphatic. aromatic and heterocyclic types are widely used by the scientific. military and commercial arts for many purposes. Often. the successful use of these chemical eonr positions necessitates their manufacture by castin molding. extruding and like processes into items of predetermined shape and design. These manufacturing processes frequently require a mixing of the energetic explosive or propellant compound with a processing agent for fabricating the desired article. For example. the manufacture of many ordnance projectiles. cartridges for small arms. blasting and demolition explosives. the casting of a shaped propellant grain into a combustion chamber. and other like items demand a mixing of the explosive or propellant with a processing agent or binder for facilitating casting or filling.
  • binders like asphalt. synthetic polybutadicne elastomers. reactive terminated elastomeric derivatives. polysiloxane type polymers. wax-like hydrocarbons. cellulose esters and other similar agents are used for processing purposes.
  • Another disadvantage is that most of the prior art materials generally contain little oxygen and therefore consume a portion of the explosive or propellant oxidizer to facilitatc their own combustion which results in a decreased performance for the explosive or propellant composition of matter. Thus. with this kind of binder it is often necessary to furnish a source of oxygen to overcome this inherent deficiency for the binder in the explosive or propellant charges.
  • Other disadvantages frequently evidenced by the prior art binders are their poor stor age characteristics. especially under different atmospheric conditions. such as over a temperature range of about "65F. to about 3()()F.. a low density with nonenergetic properties. their undesirable sensitivity to im pact and other like unwanted disadvantages.
  • Another object of the present invention is to provide novel energetic binders suitable for processing by casting and like techniques. high melting point explosives without lowering the energy content of the given explosive.
  • Still another object of the present invention is to provide energetic. thermally stable. impact stable. high energy monomers of the lower alkyl nitrohalo epoxide type suitable for manufacturing desired explosive and propellant systems without substantially decreasing the energy of the explosive or propellant.
  • Still another object of the present invention is to provide energetic. thermally stable. impact stable. high energy polymeric binders suitable for manufacturing desired explosive and propellant systems without substantially decreasing the energy of the explosive or propellant.
  • Still a further object of the instant invention is to provide energetic monomers and polymers that supply their own combustion oxygen.
  • Yet still a further object of the instant invention is to provide novel monomeric epoxy aliphatic esters terminated with a dinitrofluoro moiety and the polymers produced therefrom.
  • Still a further object of the subject invention is to produce unique monomeric glycidyl ethers substituted with a dinitrofluoro group and the novel polymers synthesized therefrom.
  • polymeric compounds derived from said monomers and which polymers can be represented by the following general formula:
  • R in l and (2) is a straight or branched chain lower alkylene of l to 4 carbon atoms such as methylene (CH- ethylene (CH -CH isopropylene cH-. cH.
  • I1 is a positive integer of from 4 to 25.
  • novel monomeric compounds of the present invention of the general formula wherein R is an alkylene of l to 4 carbon atoms; next. fluorinating said ether to form the unsaturated dinitrofluoroether,
  • the first step of the synthesis consists in the preparation of alkyl 2.2-dinitroethyl ether according to the procedure as set forth in The Journal of Organic Chemistry. Vol. 23. p. 8l3, 1958. This reaction consists in the addition of allyl alcohol to l.l-dinitroethylene according to the following equation:
  • the l.l-dinitroethylene is a reactive intermediate generated in situ from 2-bromo-2,2-dinitroethyl acetate, 1.2-diehloro-l. l-dinitroethanc or l.l.l-trinitroethane.
  • the 1.1- 5 dinitroethylene was generated from l.2-chloro-l.l-
  • the above described dinitroethylation, fluorination and cpoxidation reactions are carried out under normal atmospheric conditions.
  • the initial temperature of the dinitroethylation reaction was usually about l5C. to 25C. followed by agitation or stirring at room temperature for 10 to hours.
  • the beginning temperature of the fluorination process was its refluxing temperature followed by a reaction temperature of about C. to C. for about 3 to 4 hours.
  • the epoxidation reaction was carried out at itsrefluxing temperature for about I to 3 hours.
  • the above reactions were usually performed in the presence of an inert solvent. such as methylene chloride. carbon tetrachloride. chlorobenzene. chloroform or any other inert solvent that does not adversely affect the reactions.
  • novel polymeric compounds of the present invention of the general formula I H OCH CH 0 catalysts initiator ROCH C(NO, ),F
  • the polymerization process consists in weighing a quantity of monomer and introducing it into a reaction flask containing solvent. then adding a catalyst and allowing the polymerization reaction to proceed to produce the desired polymer. The course of the reaction can be followed by the disappearance of the epoxy group and the polymerization reaction can be terminated by the addition of water or any suitable quenching material.
  • the polymer is isolated from the reaction medium by first water extracting the solvent to remove the catalysts and then drying the extracted solvent and extracting the polymer with alcohol. Finally. the alcohol is evaporated to give the polymer.
  • Exemplary of the Lewis acid catalysts suitable for polymerizing the monomers are catalysts such as aluminum chloride. zinc chloride. ferric chloride. boron trifluoride. boron trifluoride hydrate. stannic chloride and like metal halides.
  • initiator compounds containing an OH group suitable for the polymerization reaction are compounds such as water. glycerine. glycols like ethylene glycol. polypropylene glycol. polyethylene glycol, mixed polyethylene polypropylene glycols, glycerol and the like.
  • Solvents suitable for the polymerization reaction.
  • the water layer was extracted with methylene chloride and the combined organic portion was then washed several times with a 10 percent so .dium thiosulfate to remove iodine. After a final water wash. the methylene chloride solution was dried over magnesium sulfate. Removal of excess methylene chloride yielded a red oil and a white solid. These materials 'were separated by crystallization of the solid from carbon tetrachloride. The white solid was found to be 1.2 diiodopropanol and the red oil was crude allyl 2.2-
  • reaction flask After pumping the flask down to 20 microns, 60.1 cc of boron trifluoride at a pressure of 100 millimeters was condensed into the reaction flask. The reaction flask was then removed from the vacuum line and gently warmed to room temperature, and, as soon as the monomer solution thawed, stirring was done with a magnetic stirring bar. The reaction was allowed to proceed for l2 hours, or, until the l 1.1 micron epoxide band in the infrared spectrum had disappeared. The samples were removed for infrared examination by first opening the reaction flasks stopcock under a nitrogen flow.
  • the side-arm stopper was removed and a sample was withdrawn with a hypodermic syringe. After completion of the reaction, approximately 10 milliliters of water was added to the reaction flask and stirring continued for several minutes. The contents of the flask were then transferred to a l-milliliter separatory funnel. After two additional water washes of the methylene chloride solution, the sample was dried over anhydrous sodium sulfate, and the sodium sulfate was washed with methylene chloride several times. The washes were combined with the decanted solution. Finally, the methylene chloride was evaporated under vacuum.
  • the polymer residue produced was dissolved in methanol and filtered through a conventional Millipore filter to remove small quantities of insoluble solids. Following vacuum removal of the methanol, the liquid polymer was dried in a vacuum oven at C. for several days. The yield of polymer was quantitative.
  • the parameters that were used to characterize the prepolymers are functionality and molecular weight. Functionality is indicative of the number of hydroxyl groups per polymer molecule and was determined by the diborane method. This method involves the reaction of diborane with prototonic material and subsequent measurement of the evolved hydrogen: 3 1-1 6 ROH 2B(OR) 6H-
  • the apparatus consists of a reaction vessel fitted with a serum cap and a manometer. The vessel contains excess diboranetetrahydrofuran solution into which the weighed, carefully dried sample is injected with a syringe. The resu1ting hydrogen evolution is then measured.
  • the method was modified somewhat in that the diboranetetrahydrofuran solution was metered onto a carefully weighed unknown sample contained in a vessel evacuated on a vacuum system. The hydrogen evolved is then removed with a Toepler pump and carefully measured. The analysis is quite rapid requiring approximately 30 minutes per sample. The method is especially suitable for epoxy compounds, and sterically hindered hydroxyl compounds. Nitro, nitrato, and other energetic groups do not interfere with the analysis. The other parameter, that is, molecular weight, was measured with the Mechrolob Vapor Phase Osmometer.
  • novel compounds of the invention prepared by the above described processes are thermally stable and very energetic.
  • the compound glycidyl 2,2-dinitro-2- fluoroethoxide has an explosive power of 1 17 as compared to trinitrotoluene with an explosive power of 100.
  • the energetic epoxy compounds of the invention can be used in pure form for their explosive effects or they can be utilized in admixtures with other explosives like nitroglycerin, pentaerythritol tetranitrate, ammonium nitrate, picric acid, trinitrotoluene and the like.
  • the novel polymers of the invention are ideally suited for casting explosives into items of predetermined and diverse geometric shapes.
  • the polymer can be loaded with a high percentage of oxidizer and fuel and then cast, and finally cured into a tough resilient explosive composition or composite propellant.
  • a castable explosive composition was formulated by intimately blending weight percent of cyclotrimethylenetrinitroamine (HMX), and 20 weight percent of the polymer of glycidyl 2,2-dinitro-2-- fluoroethanoxide. This castable composition had an explosive force 62 percent greater than TNT.
  • Another castable composition was formulated consisting of 80 weight percent HMX.
  • the energetic compounds and compositions of matter formed by mixing the compounds with other cxplo sives can be used for many other endeavors such as, oil well shooting. ordnance. demolition. incendiary compositions, rockets. projectiles and the like.
  • 'Explosive power is measured by detonation pressure.
  • the novel hydroxy-terminated prepolymers prepared herein can be curedwith conventional curing agents. Generally. about up to 5 weight percent of isocyanate type curing agent is employed for formulating the energetic compositions. Such diisocyanates as hexamethylene diisocyanate. bis-isoeyanatophenyl methane. toluene diisocyanate. 3-nitraza-l.S-pentane diisocyanate and the like will give a satisfactory cure. Energetic nitro plasticizers such as his(2.2-dinitro-Z-l'luoroethyl) formal and the like. usually in a concentration of 0 to 40 H -O-(H2-CH OH in which R is alkylene of l to 4 carbon atoms and n is an integer of from about 4 to 25.

Abstract

This invention is concerned with novel, energetic monomeric epoxy aliphatic ethers terminated with a dinitrofluoro moiety and with the polymers prepared therefrom. The monomers are of the general formula

and the polymers are of the general formula

WHEREIN R is a lower alkylene of 1 to 4 carbon atoms, and wherein n is a positive number of from 4 to 25.

Description

United States Patent V [191 Frankel et al.
[ 1 Sept. 23, 1975 Z-FLUORO-Z,Z-DINITROETHYL SUBSTITUTED POLYETHERS [75] Inventors: Milton B. Frankel, Tarzana; Edward F. Witucki, Sepulveda; David N. Vincent, Woodland Hills, all of Calif.
[73] Assignee: Rockwell International Corporation, El Segundo, Calif.
[22] Filed: May 16, 1968 [21] Appl. No.: 729,822
Primary Examiner-Leland A. Sebastian Attorney, Agent, or Firm-L. Lee Humphries; Robert M. Sperry [57] ABSTRACT This invention is concerned with novel, energetic monomeric epoxy aliphatic ethers terminated with a dinitrofluoro moiety and with the polymers prepared therefrom. The monomers are of the general formula and the polymers are of the general formula wherein R is a lower alkylene of l to 4 carbon atoms, and wherein n is a positive number of from 4 to 25.
2 Claims, No Drawings 2-FLUORO-2,2-DINITROETHYL SUBSTITUTED POLY ETHERS BACKGROUND OF THE lNVENTlON This invention relates to new and useful monomeric and polymeric compositions of matter. More particu' larly. the present invention pertains to energetic. thermally stable. organic monomers and the polymers derived therefrom and wherein said products are useful as energetic binders for formulating both explosive and propellant compositions. Specifically. the subject invention is concerned with novel. energetic. explosive. monomeric lower alkyl nitrohalo-epoxides and the polymers made from said monomeric epoxides.
Chemical explosives and propellants of the aliphatic. aromatic and heterocyclic types are widely used by the scientific. military and commercial arts for many purposes. Often. the successful use of these chemical eonr positions necessitates their manufacture by castin molding. extruding and like processes into items of predetermined shape and design. These manufacturing processes frequently require a mixing of the energetic explosive or propellant compound with a processing agent for fabricating the desired article. For example. the manufacture of many ordnance projectiles. cartridges for small arms. blasting and demolition explosives. the casting of a shaped propellant grain into a combustion chamber. and other like items demand a mixing of the explosive or propellant with a processing agent or binder for facilitating casting or filling. molding or extruding to successfully fabricate the desired commercial or military item. Presently. binders like asphalt. synthetic polybutadicne elastomers. reactive terminated elastomeric derivatives. polysiloxane type polymers. wax-like hydrocarbons. cellulose esters and other similar agents are used for processing purposes.
However. serious disadvantages are frequently encountered with present day binders for compounding explosive compositions and propellant grains. For example. one disadvantagc often encountered with high melting point explosives is that they cannot be safely melt cast because some decomposition occurs before they reach their melting points. To overcome this disadvantage the high melting point explosives are conventionally mixed with a castable plastic essentially nonencrgetic binder. for example. a synthetic polyester for casting the desired item. The use ofthese inert. noncnergetic synthetic binders has the definite disadvantage of lowering the total energy content of the formulated composition with a resultant decrease in energy performance for the given explosive system. Another disadvantage is that most of the prior art materials generally contain little oxygen and therefore consume a portion of the explosive or propellant oxidizer to facilitatc their own combustion which results in a decreased performance for the explosive or propellant composition of matter. Thus. with this kind of binder it is often necessary to furnish a source of oxygen to overcome this inherent deficiency for the binder in the explosive or propellant charges. Other disadvantages frequently evidenced by the prior art binders are their poor stor age characteristics. especially under different atmospheric conditions. such as over a temperature range of about "65F. to about 3()()F.. a low density with nonenergetic properties. their undesirable sensitivity to im pact and other like unwanted disadvantages.
Accordingly. it is an object of the present invention to make available to the art energetic binders with improved thermal and impact stability and density. to preserve the cnergy of explosive systems.
Another object of the present invention is to provide novel energetic binders suitable for processing by casting and like techniques. high melting point explosives without lowering the energy content of the given explosive.
Still another object of the present invention is to provide energetic. thermally stable. impact stable. high energy monomers of the lower alkyl nitrohalo epoxide type suitable for manufacturing desired explosive and propellant systems without substantially decreasing the energy of the explosive or propellant.
Still another object of the present invention is to provide energetic. thermally stable. impact stable. high energy polymeric binders suitable for manufacturing desired explosive and propellant systems without substantially decreasing the energy of the explosive or propellant.
Still a further object of the instant invention is to provide energetic monomers and polymers that supply their own combustion oxygen.
Yet still a further object of the instant invention is to provide novel monomeric epoxy aliphatic esters terminated with a dinitrofluoro moiety and the polymers produced therefrom.
Still a further object of the subject invention is to produce unique monomeric glycidyl ethers substituted with a dinitrofluoro group and the novel polymers synthesized therefrom.
Other objects and advantages of the invention will become apparent from the following detailed description and the accompanying claims.
SUMMARY OF THE INVENTION Briefly. the present invention is concerned with (1) novel energetic. monomeric compounds which can be represented by the following general formula:
CH- CH-R-O-CH:C(NO l F.
and with (2) novel energetic. polymeric compounds derived from said monomers and which polymers can be represented by the following general formula:
H o -cH. cH and wherein R in l and (2) is a straight or branched chain lower alkylene of l to 4 carbon atoms such as methylene (CH- ethylene (CH -CH isopropylene cH-. cH.
isobutylene and the like. and wherein I1 is a positive integer of from 4 to 25.
DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS The novel monomeric compounds of the present invention of the general formula wherein R is an alkylene of l to 4 carbon atoms; next. fluorinating said ether to form the unsaturated dinitrofluoroether,
and finally, direct oxidation of the olefin to the cpoxide with peracids. as depicted by the chemical reaction:
NO; NO,
NO, NO,
dinitro-2-fluoroethoxide. The first step of the synthesis consists in the preparation of alkyl 2.2-dinitroethyl ether according to the procedure as set forth in The Journal of Organic Chemistry. Vol. 23. p. 8l3, 1958. This reaction consists in the addition of allyl alcohol to l.l-dinitroethylene according to the following equation:
The l.l-dinitroethylene is a reactive intermediate generated in situ from 2-bromo-2,2-dinitroethyl acetate, 1.2-diehloro-l. l-dinitroethanc or l.l.l-trinitroethane. For the synthesis described herein. the 1.1- 5 dinitroethylene was generated from l.2-chloro-l.l-
dinitroethane according to the procedure as set forth in The Journal of Organic Chemistry. Vol. 31. p. 369. 1966.
The next step in the synthesis is the'fluorination of allyl 2.2-dinitroethyl ether with 'pcrchloryl fluoride to form the corresponding allyl 2.2-dinitro-Z-fluoroethyl ether which fluorination can be represented by the reaction H(NO ,CCH. ,OCH CH=CH FClO F(NO CCH OCH. ,CH=CH The final step of the synthesis consists in the cpoxida- 20 tion of the allyl 2.Z-dinitro-Z-fluoroethyl ether with pcroxytrifluoroacetie acid to form the desired glycidyl 2.2-dinitro-2-fluoroethoxidet The cpoxidation reaction can be represented by the equation Additional compositions of matter caneasily be prepared by the above described synthesis by employing a suitable alcohol such as 3-butene-l-ol or 2-methyl-3- butene-l-ol.
Generally, the above described dinitroethylation, fluorination and cpoxidation reactions are carried out under normal atmospheric conditions. The initial temperature of the dinitroethylation reaction was usually about l5C. to 25C. followed by agitation or stirring at room temperature for 10 to hours. The beginning temperature of the fluorination process was its refluxing temperature followed by a reaction temperature of about C. to C. for about 3 to 4 hours. The epoxidation reaction was carried out at itsrefluxing temperature for about I to 3 hours. The above reactions were usually performed in the presence of an inert solvent. such as methylene chloride. carbon tetrachloride. chlorobenzene. chloroform or any other inert solvent that does not adversely affect the reactions.
The novel polymeric compounds of the present invention of the general formula I H OCH CH 0 catalysts initiator ROCH C(NO, ),F
wherein R was as defined supra.
Briefly. the polymerization process consists in weighing a quantity of monomer and introducing it into a reaction flask containing solvent. then adding a catalyst and allowing the polymerization reaction to proceed to produce the desired polymer. The course of the reaction can be followed by the disappearance of the epoxy group and the polymerization reaction can be terminated by the addition of water or any suitable quenching material. The polymer is isolated from the reaction medium by first water extracting the solvent to remove the catalysts and then drying the extracted solvent and extracting the polymer with alcohol. Finally. the alcohol is evaporated to give the polymer.
Exemplary of the Lewis acid catalysts suitable for polymerizing the monomers are catalysts such as aluminum chloride. zinc chloride. ferric chloride. boron trifluoride. boron trifluoride hydrate. stannic chloride and like metal halides.
Representative of initiator compounds containing an OH group suitable for the polymerization reaction are compounds such as water. glycerine. glycols like ethylene glycol. polypropylene glycol. polyethylene glycol, mixed polyethylene polypropylene glycols, glycerol and the like.
Solvents. suitable for the polymerization reaction.
.generally include methylene chloride. carbon tetrachloride. ethylene chloride. methylene dichloride. methyl bromide. propyl chloride and like hydrocarbon solvents.
The above discussion is merely illustrative of the mode and manner of carrying out the present invention. and it is to be understood that the discussion is not intended to be limited to the instant disclosure. as other techniques may be successfully employed.
The following examples are representative of embodiments of the present invention and these examples are not to be construed limiting as other obvious em bodiments will be readily apparent to those versed in the art.
EXAMPLE 1 Preparation of allyl 2.2-dinitroethyl ether: 50 grams (0.264 mole) of 1.2 dichloro-l.l dinitrocthane were added dropwise over a minute period to a well stirred mixture of 200 ml of methylene chloride. 85.5 grams (1.48 moles) of allyl alcohol and 219 grams 1.32 moles) of potassium iodide. The slightly exother' mic reaction was controlled at -25C. with an ice bath. The resulting red solution was stirred at room ltempcrature for 12 hours. About 200 ml of water was added to dissolve the inorganic salts and the layers were separated. The water layer was extracted with methylene chloride and the combined organic portion was then washed several times with a 10 percent so .dium thiosulfate to remove iodine. After a final water wash. the methylene chloride solution was dried over magnesium sulfate. Removal of excess methylene chloride yielded a red oil and a white solid. These materials 'were separated by crystallization of the solid from carbon tetrachloride. The white solid was found to be 1.2 diiodopropanol and the red oil was crude allyl 2.2-
dinitroethyl ether. The crude allyl 2.2-dinitroethyl ether was purified by first forming the potassium salt through reaction with potassium hydroxide. recrystallization from methanol. and then acidifying to pH of 1 with hydrochloric acid. The resulting pure allyl 2.2- dinitroethyl ether. was obtained in 55 percent overall yield as a colorless 011.11,, 1.4527. 41' 1.3. The calculated elemental analysis for C,-,.H,.N- ,O.-, was C. 34.09: H. 4.55; N. 15.19. The found analysis was C. 34.20; H. 4.29; N. 16.11. Infrared spectrum for the compound. in Nujol. exhibited maximum peaks at 6.35. 7.5. and 9.0 microns.
EXAMPLE 11 Preparation of allyl 2.2-dinitro-2-f1uoroethyl ether: The pure allyl 2.2-dinitroethyl ether. prepared according to the procedure set forth in Example 1. was added (4.1 1 grams; 0.0234 moles) slowly to a well stirred solution of sodium hydroxide (0935 grams; 0.0234 mole) water (15 mls) and methanol (35 mls). The slightly exothermic reaction yielded an immediate orange color; the final pH was approximately 8. Perehloryl fluoride was then metered into the system to which was added a dry ice reflux condenser to prevent excess perchloryl fluoride from sweeping out of the reaction flask. When the perchloryl fluoride began to reflux vigorously. it was shut off and under slight nitrogen flow reflux was maintained for about 4 hours. The reac tion temperature was maintained between 2025C. with a water bath. The reaction mixture had changed from deep orange to pale orange in color. Water (50 mls) was added and a yellow oil dropped out of solution. The mixture was then extracted with 3-60 ml portions of methylene chloride. The methylene chloride extracts were washed with 3-30 ml portions of 3 per cent sodium hydroxide and finally with water. After dryings with magnesium sulfate. excess methylene chloride was removed under vacuum and the residual liquid was distilled through a. small Vigreux column. The distillation yielded 2.4 grams (53 percent yield) of allyl. 2,2-dinitro-2-fluoroethyl ether b.p. 42C./1.1 mm, 11,, 1.4240. (F 1.28. The calculated elemental analysis for C H N O was C. 30.93; H. 3.64; N. 14.43. The found analysis was C. 30.86; H. 3.45; N. 14.43. The infrared spectrum for the compound. in Nujol. exhibited maximum peaks at 6.2, 7.6 and 9.0 microns.
EXAMPLE Ill Preparation of glycidyl 2.Z-dinitro-2-fluoroethoxide: A solution of peroxytrifluoroacetie acid was prepared from 0.78 ml (0.028 mole) of percent hydrogen peroxide. 4.73 ml (0.0335 mole) of trifluoroacetic anhydride and 10 ml of methylene chloride. This reagent was added over a 25 minute period to a well stirred boiling mixture of 3.18 g. (0.0164 mole) of allyl 2.2-dinitro-2-fluoroethyl ether. 25 ml methylene chloride. and 12.4 g. (0.088 mole) of disodium hydrogen phosphate (pre-dried in vacuum oven overnight at 50C.). After the mild exothermic reaction had subsided, the solution was heated under reflux for 2 additional hours. The resulting mixture was stirred with 60 m1 of water until all the inorganic salts had dissolved. The organic layer was separated and the aqueous layer was extracted with 3-25 m1 portions of methylene chloride. The combined methylene chloride portion was washed with 50 ml of 10 percent sodium bicarbonate and dried over magnesium sulfate. The solvent was removed at reduced pressure and the residual liquid was fractionated through a small Vigreux column to yield 1.99 g. (58 percent yield) of glycidyl 2.2-dinitro-2- fluoroethoxide b.p. 66C./O.l5 mm, 11,, 1.4350. J 1.45. The calculated elemental analysis for C -,H N. ,O,;F was C, 28.6; H, 3.36; N, 13.33. The found analysis was C, 28.78; H, 3.29; N, 13.46. The infrared spectrum for the compound, in Nujol, exhibited maximum peaks at 6.25, 7.65, 9.4 and 11.10 microns.
EXAMPLE IV Polymerization of glycidyl 2.2-dinitro-2 fluoroethoxide: To a reaction flask. consisting of a twonecked 100-milliliter round-bottom flask wherein one neck was fitted with a 4-millimeter vacuum stopcock and the other neck stoppered for use in the introduction and removal of reagents and samples, was added 1.50 grams (7.13 mmoles) of glycidyl 2,2-dinitro-2- fluoroethoxide and milliliters of methylene chloride. The contents of the flask were next frozen in a liquid nitrogen bath, and the flask was opened to the vacuum line. After pumping the flask down to 20 microns, 60.1 cc of boron trifluoride at a pressure of 100 millimeters was condensed into the reaction flask. The reaction flask was then removed from the vacuum line and gently warmed to room temperature, and, as soon as the monomer solution thawed, stirring was done with a magnetic stirring bar. The reaction was allowed to proceed for l2 hours, or, until the l 1.1 micron epoxide band in the infrared spectrum had disappeared. The samples were removed for infrared examination by first opening the reaction flasks stopcock under a nitrogen flow. and after the contents of the flask were blanketed with nitrogen, the side-arm stopper was removed and a sample was withdrawn with a hypodermic syringe. After completion of the reaction, approximately 10 milliliters of water was added to the reaction flask and stirring continued for several minutes. The contents of the flask were then transferred to a l-milliliter separatory funnel. After two additional water washes of the methylene chloride solution, the sample was dried over anhydrous sodium sulfate, and the sodium sulfate was washed with methylene chloride several times. The washes were combined with the decanted solution. Finally, the methylene chloride was evaporated under vacuum. The polymer residue produced was dissolved in methanol and filtered through a conventional Millipore filter to remove small quantities of insoluble solids. Following vacuum removal of the methanol, the liquid polymer was dried in a vacuum oven at C. for several days. The yield of polymer was quantitative.
EXAMPLE V Other polymers of this invention were prepared according to the procedure of Example 1V and they are set forth in Table 1 immediately below:
Table 1 POLYMERIZATION OF GLYCIDYL 2.2-D1N1TRO-2-FLUOROETHOX[DE Table l-Continued POLYMERIZATION ()F (iLYClDYl. 2.2-DlNlTRO-2-Fl.UOROETHOXIDE Monomcr/ Catalyst H O/BF; Temper- Functionality M,, (Molar) (2) (Molar) aturc (4) 22:1 1.0 RT 0.58 1157 11:1 0.5 71 0.66 1643 22:1 100 RT 850 5.511 0.67 RT 0.85 1311 22:1 0.076 RT 0.57 866 22:1 0.11 RT 1.5 2660 12:1 10.0 RT 1.9 7144 22:1 50 RT 1.6 1060 22:1 029" RT 1.2 2460 Strong OH in infrared.
"'Solrenl as carbon tetrachloride. all other runs carried out in methylene chloride solvent.
12) Catalyst as 1.e\\is acid 13F (31 Functionalit indicates the average number of OH groups per pol mer chain.
(4) M,, indicates the average molecular weight of the polymer.
The parameters that were used to characterize the prepolymers are functionality and molecular weight. Functionality is indicative of the number of hydroxyl groups per polymer molecule and was determined by the diborane method. This method involves the reaction of diborane with prototonic material and subsequent measurement of the evolved hydrogen: 3 1-1 6 ROH 2B(OR) 6H- The apparatus consists of a reaction vessel fitted with a serum cap and a manometer. The vessel contains excess diboranetetrahydrofuran solution into which the weighed, carefully dried sample is injected with a syringe. The resu1ting hydrogen evolution is then measured. The method was modified somewhat in that the diboranetetrahydrofuran solution was metered onto a carefully weighed unknown sample contained in a vessel evacuated on a vacuum system. The hydrogen evolved is then removed with a Toepler pump and carefully measured. The analysis is quite rapid requiring approximately 30 minutes per sample. The method is especially suitable for epoxy compounds, and sterically hindered hydroxyl compounds. Nitro, nitrato, and other energetic groups do not interfere with the analysis. The other parameter, that is, molecular weight, was measured with the Mechrolob Vapor Phase Osmometer.
The novel compounds of the invention prepared by the above described processes are thermally stable and very energetic. The compound glycidyl 2,2-dinitro-2- fluoroethoxide has an explosive power of 1 17 as compared to trinitrotoluene with an explosive power of 100. The energetic epoxy compounds of the invention can be used in pure form for their explosive effects or they can be utilized in admixtures with other explosives like nitroglycerin, pentaerythritol tetranitrate, ammonium nitrate, picric acid, trinitrotoluene and the like.
The novel polymers of the invention are ideally suited for casting explosives into items of predetermined and diverse geometric shapes. The polymer can be loaded with a high percentage of oxidizer and fuel and then cast, and finally cured into a tough resilient explosive composition or composite propellant. For example, a castable explosive composition was formulated by intimately blending weight percent of cyclotrimethylenetrinitroamine (HMX), and 20 weight percent of the polymer of glycidyl 2,2-dinitro-2-- fluoroethanoxide. This castable composition had an explosive force 62 percent greater than TNT. Another castable composition was formulated consisting of 80 weight percent HMX. 10 weight percent of a polymer of 2.Z-dinitro-Z-fluoroethanoxide and 10 weight percent of a plasticizer his (2.2-dinitro-Z-t'luoroethyl) formal. This explosive composition had an explosive force 67 percent greater than TNT.
In Table II. immediately below. is further set forth the unobvious and unexpected results obtained by formulating explosive compositions employing binders made according to the mode and manner of the instant invention. The explosive power obtained for a composition consisting essentially of HMX and a non-energetic binder polyhutadiene. and the explosive power obtained for a composition consisting essentially of HMX and an energetic binder poly(glyeidyl 2,2-dinitro2- fluoroethanoxide) are compared against the explosive power of the standard reference explosive TNT.
weight percent. will give acceptable working properties.
The energetic compounds and compositions of matter formed by mixing the compounds with other cxplo sives can be used for many other endeavors such as, oil well shooting. ordnance. demolition. incendiary compositions, rockets. projectiles and the like.
Obviously. many modifications and variations of the instant invention are possible in the light of the above teaching. It is, therefore, to be understood that within the scope of the disclosure and appended claims. the invention may be practiced otherwise than as specifically described.
We claim:
1. A polymer of the formula "Commercially available carhoxy-terminated polybutadiene. Poly(glycidyl 2.2dinitro-Z-lluomelhanoxidel. Bis-(2.2-dinilro-2-fluoroelhyl) formal.
'Explosive power is measured by detonation pressure.
The novel hydroxy-terminated prepolymers prepared herein can be curedwith conventional curing agents. Generally. about up to 5 weight percent of isocyanate type curing agent is employed for formulating the energetic compositions. Such diisocyanates as hexamethylene diisocyanate. bis-isoeyanatophenyl methane. toluene diisocyanate. 3-nitraza-l.S-pentane diisocyanate and the like will give a satisfactory cure. Energetic nitro plasticizers such as his(2.2-dinitro-Z-l'luoroethyl) formal and the like. usually in a concentration of 0 to 40 H -O-(H2-CH OH in which R is alkylene of l to 4 carbon atoms and n is an integer of from about 4 to 25.
2. The polymer of claim 1 in which R is methylene.
l l l

Claims (2)

1. A POLYMER OF THE FORMULA
2. The polymer of claim 1 in which R is methylene.
US729822A 1968-05-16 1968-05-16 2-Fluoro-2,2-dinitroethyl substituted polyethers Expired - Lifetime US3907907A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US729822A US3907907A (en) 1968-05-16 1968-05-16 2-Fluoro-2,2-dinitroethyl substituted polyethers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US729822A US3907907A (en) 1968-05-16 1968-05-16 2-Fluoro-2,2-dinitroethyl substituted polyethers

Publications (1)

Publication Number Publication Date
US3907907A true US3907907A (en) 1975-09-23

Family

ID=24932779

Family Applications (1)

Application Number Title Priority Date Filing Date
US729822A Expired - Lifetime US3907907A (en) 1968-05-16 1968-05-16 2-Fluoro-2,2-dinitroethyl substituted polyethers

Country Status (1)

Country Link
US (1) US3907907A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4341712A (en) * 1977-02-17 1982-07-27 Rockwell International Corporation Fluorodinitro compounds
US4514341A (en) * 1984-04-19 1985-04-30 The United States Of America As Represented By The Secretary Of The Army Storage stable nitroglycerin
US4560779A (en) * 1982-07-20 1985-12-24 The United States Of America As Represented By The Secretary Of The Air Force Preparation and polymerization of oxether-1
US4855508A (en) * 1987-09-04 1989-08-08 The United States Of America As Represented By The Secretary Of The Air Force Energetic diethers and process for their preparation
US5061330A (en) * 1982-11-01 1991-10-29 The United States Of America As Represented By The Secretary Of The Navy Insensitive high energetic explosive formulations
US5256220A (en) * 1979-12-03 1993-10-26 The United States Of America As Represented By The Secretary Of The Navy Liquid monopropellants
EP0614862A1 (en) * 1993-03-12 1994-09-14 Rockwell International Corporation High-density insensitive explosives
US5587553A (en) * 1994-11-07 1996-12-24 Thiokol Corporation High performance pressable explosive compositions
US8318959B1 (en) * 2012-01-04 2012-11-27 Flurochem, Inc. Synthesis and polymerization of glycidyl ethers

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3316292A (en) * 1962-07-27 1967-04-25 Aerojet General Co Fluorodinitroalkyl esters of monocarboxylic acids and their preparation
US3652600A (en) * 1969-11-26 1972-03-28 Us Navy 2-fluoro-2 2-dinitroethyl glycidyl ether

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3316292A (en) * 1962-07-27 1967-04-25 Aerojet General Co Fluorodinitroalkyl esters of monocarboxylic acids and their preparation
US3652600A (en) * 1969-11-26 1972-03-28 Us Navy 2-fluoro-2 2-dinitroethyl glycidyl ether

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4341712A (en) * 1977-02-17 1982-07-27 Rockwell International Corporation Fluorodinitro compounds
US5256220A (en) * 1979-12-03 1993-10-26 The United States Of America As Represented By The Secretary Of The Navy Liquid monopropellants
US4560779A (en) * 1982-07-20 1985-12-24 The United States Of America As Represented By The Secretary Of The Air Force Preparation and polymerization of oxether-1
US5061330A (en) * 1982-11-01 1991-10-29 The United States Of America As Represented By The Secretary Of The Navy Insensitive high energetic explosive formulations
US4514341A (en) * 1984-04-19 1985-04-30 The United States Of America As Represented By The Secretary Of The Army Storage stable nitroglycerin
US4855508A (en) * 1987-09-04 1989-08-08 The United States Of America As Represented By The Secretary Of The Air Force Energetic diethers and process for their preparation
EP0614862A1 (en) * 1993-03-12 1994-09-14 Rockwell International Corporation High-density insensitive explosives
US5587553A (en) * 1994-11-07 1996-12-24 Thiokol Corporation High performance pressable explosive compositions
US8318959B1 (en) * 2012-01-04 2012-11-27 Flurochem, Inc. Synthesis and polymerization of glycidyl ethers

Similar Documents

Publication Publication Date Title
US4141768A (en) Fuel rich solid propellant of boron and a fluoro-nitro-epoxide polymer binder
US4707540A (en) Nitramine oxetanes and polyethers formed therefrom
Badgujar et al. New directions in the area of modern energetic polymers: An overview
US3907907A (en) 2-Fluoro-2,2-dinitroethyl substituted polyethers
EP0471489B1 (en) Process of producing improved poly(glycidyl nitrate)
EP1240234B1 (en) Polymerization of poly(glycidyl nitrate) from high purity glycidyl nitrate synthesized from glycerol
US3557181A (en) Oily polymer having polyether chain and nitroalkyl groups
Gayathri et al. Nitrato functionalized polymers for high energy propellants and explosives: recent advances
US5801325A (en) High performance large launch vehicle solid propellants
US3387044A (en) Process for fluorinating compounds containing a gem-dinitro group
US6730181B1 (en) Process for making stable cured poly(glycidyl nitrate)
US5591936A (en) Clean space motor/gas generator solid propellants
US3784420A (en) Thermally stable high density-impulse energetic composition of matter
US3523808A (en) Nitroacetal compounds
Li et al. Synthesis, Characterization and Compatibility Studies of Poly (DFAMO/NIMMO) with Propellant and PBX Ingredients
JP3067799B2 (en) Non-detonable polyglycidyl azide product
US3109031A (en) Organoboron polymers and process of making same
US3629338A (en) Certain fluoro-containing nitro-acetal compounds
US3342814A (en) Adducts of metal borohydrides and organic polynitrogen compounds
US3441518A (en) Difluoroamino epoxy alkane or cycloalkane and polymers thereof
Caro et al. Synthesis and characterization of a hydroxy terminated polyether (HTPE) copolymer for use as a binder in composite rocket propellants
US3813305A (en) High burning rate nf propellants
US3878002A (en) Nitrogen and fluorine containing solid propellant compositions based on acrylic prepolymer binders
US6861501B1 (en) Process for making stable cured poly(glycidyl nitrate) and energetic compositions comprising same
US3305569A (en) Aluminum borohydride complexes