US3305523A - Modification of telechelic-type polymers - Google Patents
Modification of telechelic-type polymers Download PDFInfo
- Publication number
- US3305523A US3305523A US221654A US22165462A US3305523A US 3305523 A US3305523 A US 3305523A US 221654 A US221654 A US 221654A US 22165462 A US22165462 A US 22165462A US 3305523 A US3305523 A US 3305523A
- Authority
- US
- United States
- Prior art keywords
- propellant
- telechelic
- polymer
- binder
- solid
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 229920000642 polymer Polymers 0.000 title description 18
- 230000004048 modification Effects 0.000 title description 3
- 238000012986 modification Methods 0.000 title description 3
- 229920002857 polybutadiene Polymers 0.000 claims description 18
- 239000005062 Polybutadiene Substances 0.000 claims description 17
- 238000006243 chemical reaction Methods 0.000 claims description 15
- 150000001875 compounds Chemical class 0.000 claims description 10
- 238000000034 method Methods 0.000 claims description 8
- MFIBZDZRPYQXOM-UHFFFAOYSA-N [dimethyl-[3-(oxiran-2-ylmethoxy)propyl]silyl]oxy-dimethyl-[3-(oxiran-2-ylmethoxy)propyl]silane Chemical compound C1OC1COCCC[Si](C)(C)O[Si](C)(C)CCCOCC1CO1 MFIBZDZRPYQXOM-UHFFFAOYSA-N 0.000 claims description 3
- OCBFFGCSTGGPSQ-UHFFFAOYSA-N [CH2]CC Chemical class [CH2]CC OCBFFGCSTGGPSQ-UHFFFAOYSA-N 0.000 claims 1
- UHUUYVZLXJHWDV-UHFFFAOYSA-N trimethyl(methylsilyloxy)silane Chemical compound C[SiH2]O[Si](C)(C)C UHUUYVZLXJHWDV-UHFFFAOYSA-N 0.000 claims 1
- 239000003380 propellant Substances 0.000 description 37
- 239000011230 binding agent Substances 0.000 description 23
- 229910052751 metal Inorganic materials 0.000 description 21
- 239000002184 metal Substances 0.000 description 21
- 239000000203 mixture Substances 0.000 description 20
- 239000004449 solid propellant Substances 0.000 description 20
- 229920006250 telechelic polymer Polymers 0.000 description 19
- -1 hydroxy radicals Chemical class 0.000 description 15
- 239000000463 material Substances 0.000 description 13
- 150000002739 metals Chemical class 0.000 description 11
- 239000002245 particle Substances 0.000 description 11
- 239000000654 additive Substances 0.000 description 10
- 239000007800 oxidant agent Substances 0.000 description 9
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 8
- 239000000446 fuel Substances 0.000 description 8
- VLTRZXGMWDSKGL-UHFFFAOYSA-N perchloric acid Chemical class OCl(=O)(=O)=O VLTRZXGMWDSKGL-UHFFFAOYSA-N 0.000 description 8
- 239000007787 solid Substances 0.000 description 8
- 229910052782 aluminium Inorganic materials 0.000 description 7
- KAKZBPTYRLMSJV-UHFFFAOYSA-N Butadiene Chemical compound C=CC=C KAKZBPTYRLMSJV-UHFFFAOYSA-N 0.000 description 6
- 125000000524 functional group Chemical group 0.000 description 6
- 239000000178 monomer Substances 0.000 description 5
- 230000008569 process Effects 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- PPBRXRYQALVLMV-UHFFFAOYSA-N Styrene Chemical compound C=CC1=CC=CC=C1 PPBRXRYQALVLMV-UHFFFAOYSA-N 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 4
- 150000004985 diamines Chemical class 0.000 description 4
- 238000002156 mixing Methods 0.000 description 4
- 238000002360 preparation method Methods 0.000 description 4
- 238000012360 testing method Methods 0.000 description 4
- GDDNTTHUKVNJRA-UHFFFAOYSA-N 3-bromo-3,3-difluoroprop-1-ene Chemical compound FC(F)(Br)C=C GDDNTTHUKVNJRA-UHFFFAOYSA-N 0.000 description 3
- OECTYKWYRCHAKR-UHFFFAOYSA-N 4-vinylcyclohexene dioxide Chemical compound C1OC1C1CC2OC2CC1 OECTYKWYRCHAKR-UHFFFAOYSA-N 0.000 description 3
- LSDPWZHWYPCBBB-UHFFFAOYSA-N Methanethiol Chemical compound SC LSDPWZHWYPCBBB-UHFFFAOYSA-N 0.000 description 3
- MUBZPKHOEPUJKR-UHFFFAOYSA-N Oxalic acid Chemical compound OC(=O)C(O)=O MUBZPKHOEPUJKR-UHFFFAOYSA-N 0.000 description 3
- YGYAWVDWMABLBF-UHFFFAOYSA-N Phosgene Chemical compound ClC(Cl)=O YGYAWVDWMABLBF-UHFFFAOYSA-N 0.000 description 3
- 230000000996 additive effect Effects 0.000 description 3
- 125000003178 carboxy group Chemical group [H]OC(*)=O 0.000 description 3
- 239000003054 catalyst Substances 0.000 description 3
- 230000008859 change Effects 0.000 description 3
- 230000006872 improvement Effects 0.000 description 3
- 239000012948 isocyanate Substances 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 3
- 230000000704 physical effect Effects 0.000 description 3
- 238000003860 storage Methods 0.000 description 3
- 229920002554 vinyl polymer Polymers 0.000 description 3
- KUDUQBURMYMBIJ-UHFFFAOYSA-N 2-prop-2-enoyloxyethyl prop-2-enoate Chemical compound C=CC(=O)OCCOC(=O)C=C KUDUQBURMYMBIJ-UHFFFAOYSA-N 0.000 description 2
- 125000003903 2-propenyl group Chemical group [H]C([*])([H])C([H])=C([H])[H] 0.000 description 2
- VVJKKWFAADXIJK-UHFFFAOYSA-N Allylamine Chemical compound NCC=C VVJKKWFAADXIJK-UHFFFAOYSA-N 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- UBJVUCKUDDKUJF-UHFFFAOYSA-N Diallyl sulfide Chemical compound C=CCSCC=C UBJVUCKUDDKUJF-UHFFFAOYSA-N 0.000 description 2
- OAKJQQAXSVQMHS-UHFFFAOYSA-N Hydrazine Chemical compound NN OAKJQQAXSVQMHS-UHFFFAOYSA-N 0.000 description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 2
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 2
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 2
- AVUYXHYHTTVPRX-UHFFFAOYSA-N Tris(2-methyl-1-aziridinyl)phosphine oxide Chemical compound CC1CN1P(=O)(N1C(C1)C)N1C(C)C1 AVUYXHYHTTVPRX-UHFFFAOYSA-N 0.000 description 2
- QYKIQEUNHZKYBP-UHFFFAOYSA-N Vinyl ether Chemical compound C=COC=C QYKIQEUNHZKYBP-UHFFFAOYSA-N 0.000 description 2
- XXROGKLTLUQVRX-UHFFFAOYSA-N allyl alcohol Chemical compound OCC=C XXROGKLTLUQVRX-UHFFFAOYSA-N 0.000 description 2
- SJNALLRHIVGIBI-UHFFFAOYSA-N allyl cyanide Chemical compound C=CCC#N SJNALLRHIVGIBI-UHFFFAOYSA-N 0.000 description 2
- 125000003277 amino group Chemical group 0.000 description 2
- IWOUKMZUPDVPGQ-UHFFFAOYSA-N barium nitrate Chemical compound [Ba+2].[O-][N+]([O-])=O.[O-][N+]([O-])=O IWOUKMZUPDVPGQ-UHFFFAOYSA-N 0.000 description 2
- 229910052790 beryllium Inorganic materials 0.000 description 2
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 2
- INLLPKCGLOXCIV-UHFFFAOYSA-N bromoethene Chemical compound BrC=C INLLPKCGLOXCIV-UHFFFAOYSA-N 0.000 description 2
- ZCCIPPOKBCJFDN-UHFFFAOYSA-N calcium nitrate Chemical compound [Ca+2].[O-][N+]([O-])=O.[O-][N+]([O-])=O ZCCIPPOKBCJFDN-UHFFFAOYSA-N 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 150000001991 dicarboxylic acids Chemical class 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- NAQMVNRVTILPCV-UHFFFAOYSA-N hexane-1,6-diamine Chemical compound NCCCCCCN NAQMVNRVTILPCV-UHFFFAOYSA-N 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N iron oxide Inorganic materials [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 description 2
- 229910052744 lithium Inorganic materials 0.000 description 2
- IIPYXGDZVMZOAP-UHFFFAOYSA-N lithium nitrate Chemical compound [Li+].[O-][N+]([O-])=O IIPYXGDZVMZOAP-UHFFFAOYSA-N 0.000 description 2
- 238000011068 loading method Methods 0.000 description 2
- YIXJRHPUWRPCBB-UHFFFAOYSA-N magnesium nitrate Chemical compound [Mg+2].[O-][N+]([O-])=O.[O-][N+]([O-])=O YIXJRHPUWRPCBB-UHFFFAOYSA-N 0.000 description 2
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 2
- 229910044991 metal oxide Inorganic materials 0.000 description 2
- 150000004706 metal oxides Chemical class 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- NDLPOXTZKUMGOV-UHFFFAOYSA-N oxo(oxoferriooxy)iron hydrate Chemical compound O.O=[Fe]O[Fe]=O NDLPOXTZKUMGOV-UHFFFAOYSA-N 0.000 description 2
- 230000000737 periodic effect Effects 0.000 description 2
- 229920003023 plastic Polymers 0.000 description 2
- 239000004033 plastic Substances 0.000 description 2
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 2
- 239000002491 polymer binding agent Substances 0.000 description 2
- 238000006116 polymerization reaction Methods 0.000 description 2
- FGIUAXJPYTZDNR-UHFFFAOYSA-N potassium nitrate Chemical compound [K+].[O-][N+]([O-])=O FGIUAXJPYTZDNR-UHFFFAOYSA-N 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 230000035484 reaction time Effects 0.000 description 2
- 229910052709 silver Inorganic materials 0.000 description 2
- 239000004332 silver Substances 0.000 description 2
- VWDWKYIASSYTQR-UHFFFAOYSA-N sodium nitrate Chemical compound [Na+].[O-][N+]([O-])=O VWDWKYIASSYTQR-UHFFFAOYSA-N 0.000 description 2
- DHEQXMRUPNDRPG-UHFFFAOYSA-N strontium nitrate Chemical compound [Sr+2].[O-][N+]([O-])=O.[O-][N+]([O-])=O DHEQXMRUPNDRPG-UHFFFAOYSA-N 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 125000000391 vinyl group Chemical group [H]C([*])=C([H])[H] 0.000 description 2
- VFRMAHVDXYSEON-UHFFFAOYSA-N 1,1-diiodoethene Chemical compound IC(I)=C VFRMAHVDXYSEON-UHFFFAOYSA-N 0.000 description 1
- YKLWPGCWVBBCTO-UHFFFAOYSA-N 1-ethenoxyprop-1-ene Chemical compound CC=COC=C YKLWPGCWVBBCTO-UHFFFAOYSA-N 0.000 description 1
- SDRZFSPCVYEJTP-UHFFFAOYSA-N 1-ethenylcyclohexene Chemical group C=CC1=CCCCC1 SDRZFSPCVYEJTP-UHFFFAOYSA-N 0.000 description 1
- IDCPFAYURAQKDZ-UHFFFAOYSA-N 1-nitroguanidine Chemical compound NC(=N)N[N+]([O-])=O IDCPFAYURAQKDZ-UHFFFAOYSA-N 0.000 description 1
- WHQOKFZWSDOTQP-UHFFFAOYSA-N 2,3-dihydroxypropyl 4-aminobenzoate Chemical compound NC1=CC=C(C(=O)OCC(O)CO)C=C1 WHQOKFZWSDOTQP-UHFFFAOYSA-N 0.000 description 1
- VOZKAJLKRJDJLL-UHFFFAOYSA-N 2,4-diaminotoluene Chemical compound CC1=CC=C(N)C=C1N VOZKAJLKRJDJLL-UHFFFAOYSA-N 0.000 description 1
- STMDPCBYJCIZOD-UHFFFAOYSA-N 2-(2,4-dinitroanilino)-4-methylpentanoic acid Chemical compound CC(C)CC(C(O)=O)NC1=CC=C([N+]([O-])=O)C=C1[N+]([O-])=O STMDPCBYJCIZOD-UHFFFAOYSA-N 0.000 description 1
- PAWQVTBBRAZDMG-UHFFFAOYSA-N 2-(3-bromo-2-fluorophenyl)acetic acid Chemical compound OC(=O)CC1=CC=CC(Br)=C1F PAWQVTBBRAZDMG-UHFFFAOYSA-N 0.000 description 1
- OEPOKWHJYJXUGD-UHFFFAOYSA-N 2-(3-phenylmethoxyphenyl)-1,3-thiazole-4-carbaldehyde Chemical compound O=CC1=CSC(C=2C=C(OCC=3C=CC=CC=3)C=CC=2)=N1 OEPOKWHJYJXUGD-UHFFFAOYSA-N 0.000 description 1
- ULIKDJVNUXNQHS-UHFFFAOYSA-N 2-Propene-1-thiol Chemical compound SCC=C ULIKDJVNUXNQHS-UHFFFAOYSA-N 0.000 description 1
- PHMRPWPDDRGGGF-UHFFFAOYSA-N 2-bromoprop-1-ene Chemical compound CC(Br)=C PHMRPWPDDRGGGF-UHFFFAOYSA-N 0.000 description 1
- PNLQPWWBHXMFCA-UHFFFAOYSA-N 2-chloroprop-1-ene Chemical compound CC(Cl)=C PNLQPWWBHXMFCA-UHFFFAOYSA-N 0.000 description 1
- NGOCAPPEAVAHQM-UHFFFAOYSA-N 2-fluoroprop-1-ene Chemical compound CC(F)=C NGOCAPPEAVAHQM-UHFFFAOYSA-N 0.000 description 1
- JDTUPLBMGDDPJS-UHFFFAOYSA-N 2-methoxy-2-phenylethanol Chemical compound COC(CO)C1=CC=CC=C1 JDTUPLBMGDDPJS-UHFFFAOYSA-N 0.000 description 1
- QCMKXHXKNIOBBC-UHFFFAOYSA-N 3-fluoroprop-1-ene Chemical compound FCC=C QCMKXHXKNIOBBC-UHFFFAOYSA-N 0.000 description 1
- GNSFRPWPOGYVLO-UHFFFAOYSA-N 3-hydroxypropyl 2-methylprop-2-enoate Chemical compound CC(=C)C(=O)OCCCO GNSFRPWPOGYVLO-UHFFFAOYSA-N 0.000 description 1
- RBWNDBNSJFCLBZ-UHFFFAOYSA-N 7-methyl-5,6,7,8-tetrahydro-3h-[1]benzothiolo[2,3-d]pyrimidine-4-thione Chemical compound N1=CNC(=S)C2=C1SC1=C2CCC(C)C1 RBWNDBNSJFCLBZ-UHFFFAOYSA-N 0.000 description 1
- NLHHRLWOUZZQLW-UHFFFAOYSA-N Acrylonitrile Chemical compound C=CC#N NLHHRLWOUZZQLW-UHFFFAOYSA-N 0.000 description 1
- OSDWBNJEKMUWAV-UHFFFAOYSA-N Allyl chloride Chemical compound ClCC=C OSDWBNJEKMUWAV-UHFFFAOYSA-N 0.000 description 1
- XJHDWSFEGCYSFP-UHFFFAOYSA-N C=C.ClC(Cl)=O Chemical compound C=C.ClC(Cl)=O XJHDWSFEGCYSFP-UHFFFAOYSA-N 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- QPLDLSVMHZLSFG-UHFFFAOYSA-N Copper oxide Chemical compound [Cu]=O QPLDLSVMHZLSFG-UHFFFAOYSA-N 0.000 description 1
- 239000005751 Copper oxide Substances 0.000 description 1
- RWSOTUBLDIXVET-UHFFFAOYSA-N Dihydrogen sulfide Chemical class S RWSOTUBLDIXVET-UHFFFAOYSA-N 0.000 description 1
- BRLQWZUYTZBJKN-UHFFFAOYSA-N Epichlorohydrin Chemical compound ClCC1CO1 BRLQWZUYTZBJKN-UHFFFAOYSA-N 0.000 description 1
- IMROMDMJAWUWLK-UHFFFAOYSA-N Ethenol Chemical compound OC=C IMROMDMJAWUWLK-UHFFFAOYSA-N 0.000 description 1
- JIGUQPWFLRLWPJ-UHFFFAOYSA-N Ethyl acrylate Chemical compound CCOC(=O)C=C JIGUQPWFLRLWPJ-UHFFFAOYSA-N 0.000 description 1
- PIICEJLVQHRZGT-UHFFFAOYSA-N Ethylenediamine Chemical compound NCCN PIICEJLVQHRZGT-UHFFFAOYSA-N 0.000 description 1
- QIGBRXMKCJKVMJ-UHFFFAOYSA-N Hydroquinone Chemical compound OC1=CC=C(O)C=C1 QIGBRXMKCJKVMJ-UHFFFAOYSA-N 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- MPCRDALPQLDDFX-UHFFFAOYSA-L Magnesium perchlorate Chemical compound [Mg+2].[O-]Cl(=O)(=O)=O.[O-]Cl(=O)(=O)=O MPCRDALPQLDDFX-UHFFFAOYSA-L 0.000 description 1
- WSMYVTOQOOLQHP-UHFFFAOYSA-N Malondialdehyde Chemical compound O=CCC=O WSMYVTOQOOLQHP-UHFFFAOYSA-N 0.000 description 1
- BAPJBEWLBFYGME-UHFFFAOYSA-N Methyl acrylate Chemical class COC(=O)C=C BAPJBEWLBFYGME-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 239000004698 Polyethylene Substances 0.000 description 1
- OFOBLEOULBTSOW-UHFFFAOYSA-N Propanedioic acid Natural products OC(=O)CC(O)=O OFOBLEOULBTSOW-UHFFFAOYSA-N 0.000 description 1
- PCSMJKASWLYICJ-UHFFFAOYSA-N Succinic aldehyde Chemical compound O=CCCC=O PCSMJKASWLYICJ-UHFFFAOYSA-N 0.000 description 1
- WGLPBDUCMAPZCE-UHFFFAOYSA-N Trioxochromium Chemical compound O=[Cr](=O)=O WGLPBDUCMAPZCE-UHFFFAOYSA-N 0.000 description 1
- 239000007983 Tris buffer Substances 0.000 description 1
- XTXRWKRVRITETP-UHFFFAOYSA-N Vinyl acetate Chemical compound CC(=O)OC=C XTXRWKRVRITETP-UHFFFAOYSA-N 0.000 description 1
- BZHJMEDXRYGGRV-UHFFFAOYSA-N Vinyl chloride Chemical compound ClC=C BZHJMEDXRYGGRV-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 150000001252 acrylic acid derivatives Chemical class 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- BHELZAPQIKSEDF-UHFFFAOYSA-N allyl bromide Chemical compound BrCC=C BHELZAPQIKSEDF-UHFFFAOYSA-N 0.000 description 1
- 150000001412 amines Chemical class 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 1
- 239000010425 asbestos Substances 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- MEVHTHLQPUQANE-UHFFFAOYSA-N aziridine-2,3-dione Chemical compound O=C1NC1=O MEVHTHLQPUQANE-UHFFFAOYSA-N 0.000 description 1
- OOULUYZFLXDWDQ-UHFFFAOYSA-L barium perchlorate Chemical compound [Ba+2].[O-]Cl(=O)(=O)=O.[O-]Cl(=O)(=O)=O OOULUYZFLXDWDQ-UHFFFAOYSA-L 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- IISBACLAFKSPIT-UHFFFAOYSA-N bisphenol A Chemical compound C=1C=C(O)C=CC=1C(C)(C)C1=CC=C(O)C=C1 IISBACLAFKSPIT-UHFFFAOYSA-N 0.000 description 1
- OWBTYPJTUOEWEK-UHFFFAOYSA-N butane-2,3-diol Chemical compound CC(O)C(C)O OWBTYPJTUOEWEK-UHFFFAOYSA-N 0.000 description 1
- WKDKOOITVYKILI-UHFFFAOYSA-M caesium perchlorate Chemical compound [Cs+].[O-]Cl(=O)(=O)=O WKDKOOITVYKILI-UHFFFAOYSA-M 0.000 description 1
- 125000004432 carbon atom Chemical group C* 0.000 description 1
- 239000006229 carbon black Substances 0.000 description 1
- 150000001735 carboxylic acids Chemical class 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 238000001311 chemical methods and process Methods 0.000 description 1
- 150000001805 chlorine compounds Chemical class 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229920001577 copolymer Polymers 0.000 description 1
- 229910000431 copper oxide Inorganic materials 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000004132 cross linking Methods 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 150000001993 dienes Chemical class 0.000 description 1
- 125000005442 diisocyanate group Chemical group 0.000 description 1
- AXZAYXJCENRGIM-UHFFFAOYSA-J dipotassium;tetrabromoplatinum(2-) Chemical compound [K+].[K+].[Br-].[Br-].[Br-].[Br-].[Pt+2] AXZAYXJCENRGIM-UHFFFAOYSA-J 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000010419 fine particle Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- XUCNUKMRBVNAPB-UHFFFAOYSA-N fluoroethene Chemical compound FC=C XUCNUKMRBVNAPB-UHFFFAOYSA-N 0.000 description 1
- NDEMNVPZDAFUKN-UHFFFAOYSA-N guanidine;nitric acid Chemical compound NC(N)=N.O[N+]([O-])=O.O[N+]([O-])=O NDEMNVPZDAFUKN-UHFFFAOYSA-N 0.000 description 1
- LNMQRPPRQDGUDR-UHFFFAOYSA-N hexyl prop-2-enoate Chemical compound CCCCCCOC(=O)C=C LNMQRPPRQDGUDR-UHFFFAOYSA-N 0.000 description 1
- 125000004435 hydrogen atom Chemical group [H]* 0.000 description 1
- ORTFAQDWJHRMNX-UHFFFAOYSA-N hydroxidooxidocarbon(.) Chemical group O[C]=O ORTFAQDWJHRMNX-UHFFFAOYSA-N 0.000 description 1
- 125000004356 hydroxy functional group Chemical group O* 0.000 description 1
- 230000008676 import Effects 0.000 description 1
- 239000011872 intimate mixture Substances 0.000 description 1
- GHXZPUGJZVBLGC-UHFFFAOYSA-N iodoethene Chemical compound IC=C GHXZPUGJZVBLGC-UHFFFAOYSA-N 0.000 description 1
- 150000002513 isocyanates Chemical class 0.000 description 1
- 125000000555 isopropenyl group Chemical group [H]\C([H])=C(\*)C([H])([H])[H] 0.000 description 1
- 229910000464 lead oxide Inorganic materials 0.000 description 1
- MHCFAGZWMAWTNR-UHFFFAOYSA-M lithium perchlorate Chemical compound [Li+].[O-]Cl(=O)(=O)=O MHCFAGZWMAWTNR-UHFFFAOYSA-M 0.000 description 1
- 229910001486 lithium perchlorate Inorganic materials 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- VZCYOOQTPOCHFL-UPHRSURJSA-N maleic acid Chemical compound OC(=O)\C=C/C(O)=O VZCYOOQTPOCHFL-UPHRSURJSA-N 0.000 description 1
- 239000011976 maleic acid Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 150000002734 metacrylic acid derivatives Chemical class 0.000 description 1
- 229910001512 metal fluoride Inorganic materials 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 229910001960 metal nitrate Inorganic materials 0.000 description 1
- 239000003607 modifier Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- XMMDVXFQGOEOKH-UHFFFAOYSA-N n'-dodecylpropane-1,3-diamine Chemical compound CCCCCCCCCCCCNCCCN XMMDVXFQGOEOKH-UHFFFAOYSA-N 0.000 description 1
- IOXXVNYDGIXMIP-UHFFFAOYSA-N n-methylprop-2-en-1-amine Chemical compound CNCC=C IOXXVNYDGIXMIP-UHFFFAOYSA-N 0.000 description 1
- YPHQUSNPXDGUHL-UHFFFAOYSA-N n-methylprop-2-enamide Chemical compound CNC(=O)C=C YPHQUSNPXDGUHL-UHFFFAOYSA-N 0.000 description 1
- 150000002823 nitrates Chemical class 0.000 description 1
- 235000006408 oxalic acid Nutrition 0.000 description 1
- RPQRDASANLAFCM-UHFFFAOYSA-N oxiran-2-ylmethyl prop-2-enoate Chemical class C=CC(=O)OCC1CO1 RPQRDASANLAFCM-UHFFFAOYSA-N 0.000 description 1
- YEXPOXQUZXUXJW-UHFFFAOYSA-N oxolead Chemical compound [Pb]=O YEXPOXQUZXUXJW-UHFFFAOYSA-N 0.000 description 1
- AUONHKJOIZSQGR-UHFFFAOYSA-N oxophosphane Chemical compound P=O AUONHKJOIZSQGR-UHFFFAOYSA-N 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 239000013618 particulate matter Substances 0.000 description 1
- PNJWIWWMYCMZRO-UHFFFAOYSA-N pent‐4‐en‐2‐one Natural products CC(=O)CC=C PNJWIWWMYCMZRO-UHFFFAOYSA-N 0.000 description 1
- VLTRZXGMWDSKGL-UHFFFAOYSA-M perchlorate Inorganic materials [O-]Cl(=O)(=O)=O VLTRZXGMWDSKGL-UHFFFAOYSA-M 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 239000000049 pigment Substances 0.000 description 1
- 229910052697 platinum Inorganic materials 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- 229920005596 polymer binder Polymers 0.000 description 1
- 235000010333 potassium nitrate Nutrition 0.000 description 1
- 239000004323 potassium nitrate Substances 0.000 description 1
- 229910001487 potassium perchlorate Inorganic materials 0.000 description 1
- 239000012255 powdered metal Substances 0.000 description 1
- NHARPDSAXCBDDR-UHFFFAOYSA-N propyl 2-methylprop-2-enoate Chemical class CCCOC(=O)C(C)=C NHARPDSAXCBDDR-UHFFFAOYSA-N 0.000 description 1
- 125000001436 propyl group Chemical group [H]C([*])([H])C([H])([H])C([H])([H])[H] 0.000 description 1
- KIDHWZJUCRJVML-UHFFFAOYSA-N putrescine Chemical compound NCCCCN KIDHWZJUCRJVML-UHFFFAOYSA-N 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229910052895 riebeckite Inorganic materials 0.000 description 1
- 229910001489 rubidium perchlorate Inorganic materials 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 235000010344 sodium nitrate Nutrition 0.000 description 1
- 239000004317 sodium nitrate Substances 0.000 description 1
- BAZAXWOYCMUHIX-UHFFFAOYSA-M sodium perchlorate Chemical compound [Na+].[O-]Cl(=O)(=O)=O BAZAXWOYCMUHIX-UHFFFAOYSA-M 0.000 description 1
- 229910001488 sodium perchlorate Inorganic materials 0.000 description 1
- 239000011343 solid material Substances 0.000 description 1
- MXRFIUHRIOLIIV-UHFFFAOYSA-L strontium;diperchlorate Chemical compound [Sr+2].[O-]Cl(=O)(=O)=O.[O-]Cl(=O)(=O)=O MXRFIUHRIOLIIV-UHFFFAOYSA-L 0.000 description 1
- PXQLVRUNWNTZOS-UHFFFAOYSA-N sulfanyl Chemical class [SH] PXQLVRUNWNTZOS-UHFFFAOYSA-N 0.000 description 1
- 125000003698 tetramethyl group Chemical group [H]C([H])([H])* 0.000 description 1
- 239000004408 titanium dioxide Substances 0.000 description 1
- VZCYOOQTPOCHFL-UHFFFAOYSA-N trans-butenedioic acid Natural products OC(=O)C=CC(O)=O VZCYOOQTPOCHFL-UHFFFAOYSA-N 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 1
- 229920001567 vinyl ester resin Polymers 0.000 description 1
- UIYCHXAGWOYNNA-UHFFFAOYSA-N vinyl sulfide Chemical compound C=CSC=C UIYCHXAGWOYNNA-UHFFFAOYSA-N 0.000 description 1
- 239000011345 viscous material Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
- C08G59/00—Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
- C08G59/18—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
- C08G59/20—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the epoxy compounds used
- C08G59/22—Di-epoxy compounds
- C08G59/30—Di-epoxy compounds containing atoms other than carbon, hydrogen, oxygen and nitrogen
- C08G59/306—Di-epoxy compounds containing atoms other than carbon, hydrogen, oxygen and nitrogen containing silicon
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
- C06B45/04—Compositions 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
- C06B45/06—Compositions 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
- C06B45/10—Compositions 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
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08C—TREATMENT OR CHEMICAL MODIFICATION OF RUBBERS
- C08C19/00—Chemical modification of rubber
- C08C19/30—Addition of a reagent which reacts with a hetero atom or a group containing hetero atoms of the macromolecule
- C08C19/34—Addition of a reagent which reacts with a hetero atom or a group containing hetero atoms of the macromolecule reacting with oxygen or oxygen-containing groups
- C08C19/36—Addition of a reagent which reacts with a hetero atom or a group containing hetero atoms of the macromolecule reacting with oxygen or oxygen-containing groups with carboxy radicals
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L63/00—Compositions of epoxy resins; Compositions of derivatives of epoxy resins
Definitions
- This invention concerns a novel solid propellant polymeric binder. More specifically, this invention pertains to a solid propellant binder having unexpectedly high elongation properties and high solid loading ability.
- a typical composite solid propellant is comprised of solid particulate fuel such as minute particles of a metal and a solid particulate oxidizer which serves to oxidize the fuel particles.
- a resinous matrix material or binder is required.
- the binder material normally additionally serves as a fuel component of the solid propellant.
- This binder is normally a liquid resinous i material and when mixed with high percentages of the solid particles of fuel and oxidizer, forms a viscous material which may be cast in a mold and cured for the desired shaped propellant charge. Physical properties are desired in a solid propellant.
- the solid propellant should be stable for a long period of time and should not deteriorate chemically or physically during storage. High density of the solid propellant permits the use of a small chamber volume and therefore small chamber weight.
- the propellant should lend itself readily to production and have desirable fabrication properties such as adequate fluidity during casting or easy to control chemical processes such as curing and a minimal volume change after casting or molding.
- the mechanical properties and the combustion characteristics such as burning rate should be predictable and uneifected appreciably over a wide range of storage and operating temperatures. This means that the temperature sensitivity should be low.
- propellant should exhibit good mechanical properties, particularly its tensile, compressive and sheer strength and its rnodulous of elasticity and elongation. Finally the propellant should have high solids loading capability.
- the propellant binder polymer utilized is a carboxy-terminated linear polybutadiene.
- the excellent properties of the binder are attained when the starting initial molecules of butadiene have the hydrogen atoms at the double bonds in carefully ordered positions in space to obtain a symmetrical cross-linking of the cured polymer.
- the polymer has a properly controlled cistrans stereoisomerism, when the polymerization is stopped at 100 molecules of butadiene per chain, when the number or nature of possible side chains is concerned and when a carboxylic group is attached at either end of each polybutadiene molecule and nowhere else.
- the resulting symmetrical 3,305,523 Patented Feb. 21, 1967 structure has good elastorneric properties and is achieved in the binder by controlling the chemistry and of the polymerization process itself.
- This type of polybutadiene polymer is referred to as a telechelic-type polymer and the method of preparation is well known in the art and is described in the Journal of Polymer Science, vol. XLVI, Issue 148, pp. 535-539 (1960).
- An example of the carboxy-terminated polybutadiene binder used in this group of propellants is Butarez CTL manufactured by the Phillips Petroleum Company.
- other possible terminal groups can successfully be utilized in the present applications. Such other terminal functional groups would include hydroxy radicals, amine, mercapto and isocyanate radicals. It is understood that any telechelic polymer regardless of the terminal functional groups can be successfully utilized.
- the present invention concerns the further improvement of mechanical properties of the telechelic polymer binders previously described.
- the invention is directed to the improvement of the mechanical properties of the binder material over a wide range of temperature varying from less than -70 F. to excess of F.
- the greatly improved mechanical properties are accomplished in the present invention by the extension of the telechelic polymer chains through increasing the chain length and molecular Weight by the addition of from 0.4 to 10 parts by weight of difunctional materials, such as, for example, vinylcyclohexene dioxide.
- difunctional materials such as, for example, vinylcyclohexene dioxide.
- Particularly preferred is from 0.6 to 5 parts by weight of the difunctional additives.
- the difunctional additive that is utilized depends upon the functional terminal group in the telechelic polymer compound.
- the difunctional additive must be one that will react with the functional terminal group of the polymer in order for an effective result to be obtained.
- various difunctional additives may be used depending upon the functional terminal group of the telechelic polymer.
- the difunctional additive becomes part of the polymer chains.
- the elongation of the propellants utilizing the binders of this invention have increased 40 to 50 percent over a temperature range of 70 to 170 F. In some instances this represents a doubling of the percent elongation of the propellant.
- the telechelic polymers used in the propellant binder as previously described are not only polybutadienes.
- the invention also pertains to the improvement of the mechanical properties of telechelic polymers which may be of other skeletal structures such as any polymerizable monomer containing an ethylenic linkage.
- Non-limiting examples of the monomers that may be utilized in the invention to produce the telechelic polymers include the vinyl halides such as iodoethene, bromoethene, fiuorethene, chloroethene; vinylidene halides including vinylidene chloride, vinylidene iodide, and the like; vinyl esters of carboxylic acids having 1 to 10 carbon atoms including vinyl acetate and the like; and N-substituted acrylamides and methyacrylamide including N methylacrylamide, N-propyl methyacrylamide, N-hexyl aerylamide and the like; allyl and methya-llyl monomers including allylamine, N-methylallylamine, allyl bromide, allyl alcohol, allyl chloride, allyl cyanide, allyl fluoride, allyl glycidyl ether, allyl isodide, allyl mercap
- the functional terminal groups that are present can be selected from hydroxy, amino, mercapto and isocyanate radicals, in addition to any other reactive functional groups.
- the compounds which are added to the telechelic polymer to improve the mechanical properties of the propellants formed can be varied depending upon the functional terminal groups present in the telechelic polymer.
- the difunctional additives may include dialcohols such as dihydroxybenzene, dihydroxynapthaline, dihydroxybutane, and the like; diepoxides such as vinylcyclohexene dioxide, the Epon resins which are the products of epichlorohydrin and bis-phenol-A, diamines such as ethylene diamine, butylene diamine, hexamethylene diamine and the like; diamines such as hydrazine and the like; and lbis-chlorocarbonates such as ethylene bis-chlorocarbonate and the like.
- dialcohols such as dihydroxybenzene, dihydroxynapthaline, dihydroxybutane, and the like
- diepoxides such as vinylcyclohexene dioxide, the Epon resins which are the products of epichlorohydrin and bis-phenol-A
- diamines such as ethylene diamine, butylene diamine, hexamethylene diamine and the like
- diamines such as hydrazine and the like
- the difunctional additives may be selected from the group consisting of diimines; dicarboxylic acid chlorides such as succinyl chloride and the like; dicarboxylic acids such as maleic acid and the like; phosgene; bis-chlocarbonates and the like; and diisocyanates which are formed by treating diamines such as toluene 2,4-diamine, hexamethy aminediamine, and the like with phosgene.
- diimines dicarboxylic acid chlorides such as succinyl chloride and the like
- dicarboxylic acids such as maleic acid and the like
- phosgene bis-chlocarbonates and the like
- diisocyanates which are formed by treating diamines such as toluene 2,4-diamine, hexamethy aminediamine, and the like with phosgene.
- the difunctional additives may be selected from the group consisting of dicarboxylic acids; diamines; diepoxides; and dialdahydes such as malonic aldehyde and succinic aldehyde.
- the difunctional additives utilized may be acid chlorides; bischlorocarbonates; and usually any compound containing two double bonds (diolefins) capable of reacting with the mercaptan, such as ethyleneglycol diacrylate, for example. It is believed the invention will be further understood from the following detailed examples.
- the terminal difunctional additives having difunctional terminal hydroxy may be any compounds or amino groups or one of each functional type.
- Example 1 Into a two and one fourth gallon Baker-Perkins dispersion blade mixer was added 1000 grams of Butarez CTL which is a carboxy-terminated linear polybutadiene. Additionally added was 6 grams of vinylcyclohexenedioxide. Water, at 165 F., was circulated through the mixer heating jacket. The material was then blended for fifteen minutes. A 28-inch vacuum was then applied and mixing continued for an additional ten minutes to remove the air present. The contents of the mixer were then poured into a large polyethylene bag. The bag was then sealed and then placed in a metal bucket container, the bag serving two functions. (1) To prevent contact with metal surfaces and (2) to prevent contact with air. The material was then heated for 168 hours at 170 F.
- a liquid modified polymer of this invention was obtained upon cooling of the material at room temperature and the removal from the sealed bag. The above procedure was repeated utilizing 1000 grams of the Butarez CTL and 10 grams of 1,3-bis[3 (2,3-epoxy-propoxy)propyl]tetra methyl disiloxane. A modified telechelic polymer of this .invention was obtained.
- the temperature and length of time of reaction varies considerably.
- the temperature of reaction may vary from, for example, 15 0 F. to 225 F. with the time of reaction varying according to the temperature utilized with the higher temperatures requiring less reaction time.
- reaction times can vary from 145 hours to hours. Basically more important than the temperature and time of reaction ,is the assurance of conversion to the desired product.
- samples of the mixture are taken from time to time during the reaction period. The samples are analyzed, for example, in the case of the carboxy-terminated telechelic polymers to determine the ephr value, that is the carboxyl equivalents.
- the invention has peculiar applicability to the field of solid propellants wherein the polymers are used as binders to secure the solid particulate matter utilized.
- the solid material which may be dispersed throughout the polymer matrix is usually in finely divided form having a particle size ranging from about 1-500 microns or greater in diameter.
- the composition is intended as a solid propellant grain, it is often desirable to employ a combination of two or more different particle size ranges.
- solid propellants are prepared in which the finer material comprises a fine particle size range of from 1 to about 75 microns and a coarse range of from about 75 to 500.
- particles of any size within the range of 1500 microns may be employed without regard to particle size. This gives desirable burning rates to the propellant.
- the particle size ranges may be adjusted depending upon the particular binder-fueloxidizer combination employed and the specific impulse desired.
- the solid substances with which the polymeric materials are loaded may be inert pigments such as titanium dioxide, lead oxide, ferric oxide, carbon black, powdered metals and alloys, metal fluorides, asbestos fibers, etc.
- the solids When the solids are oxidizing agents, they can be compounds such as metal perchlorates and metal nitrates.
- the metal perchlorates employed as oxidizing agents or oxygen carriers in the compositions are anhydrous and have the general formula M(ClO wherein M is NH or a metal and x is the valence of M. Since the propellant composition is required to withstand high temperature storage, it is preferable that the melting point and the decomposition temperature of the oxidizer be as high as possible.
- the perchlorates of the Group I-A, Group- I-B, and Group II-A metals are found to have the re-- quired high temperature stability and are employed in the preparation of propellant compositions by the process of this invention.
- the metal perchlorates used in the preparation of the propellant compositions include lithium perchlorate, sodium perchlorate, potassium perchlorate, rubidium perchlorate, and cesium perchlorate which are the perchlorates of the metals of Group I-A of the Periodic Table of Elements; silver perchlorate which is a perchlorate of the Group IB metal; and magnesium perchlorate, calcium perchlorate, strontium perchlorate, and barium perchlorate which are the perchlorates of the Group II-A metals.
- the compound ammonium perchlorate finds extensive use in propellant compositions.
- nitrates of the Group IA, and I-B and II-B which are employed in preparing propellant compositions by the process of this invention are compounds such as lithium nitrate, sodium nitrate, potassium nitrate, magnesium nitrate, calcium nitrate, barium nitrate, strontium nitrate, etc; Ammonium nitrate is also used.
- the ratio of total solids-to-polymeric binder material in a propellant falls in the range of from about 1:1 to about 9:1 with an optimum ratio of about 85:15.
- burning catalysts well known in propellant compositions. These are composed of one or a mixture of two or more metal oxide powders in amounts suificient to improve the burning rate of the composition. The amounts usually range from about 0.01 to about 3 weight percent, based on the weight of the oxidizer employed. The particle size of the powders can range from about 10 to about 250 microns in diameter.
- metals that serve as burning catalysts are copper, vanadium, chromium, silver, molybdenum, sinconium, antimony, manganese, iron, cobalt, and nickel.
- metal oxide burning catalysts are ferric oxide, aluminum, copper oxide, chromic oxide, as well as the oxides of the other metals mentioned above.
- the fuel particles that are employed in a solid propellant grain are usually a metal or a metal alloy, preferably the fuel contains 1 or more metals of groups I-A, II-A, III-A and groups I-B through VII-B, group III of the Periodic Table.
- the metals may contain group I-A elements such as lithium and group IIA metals such as beryllium or magnesium.
- group III-A metals is aluminum.
- the metals of groups I-B through VII-B include copper, silver, zinc, manganese, iron, nickel, platinum and the like.
- Particularly preferred for inclusion in the polymer matrix are aluminum, beryllium and lithium since these metals are of relatively low molecular weight giving low molecular weight combustion products in addition to having high heats of combustion.
- Burning rate depressants and modifiers are also sometimes advantageously added to the solid propellant grain of this invention. These are generally compounds which tend to inhibit burning reaction rates or absorb heat and include specifically carbonyl chloride, oximide, nitroguanidine, guanidine nitrate, and oxalic acid.
- the improved properties obtained by the modification of a telechelic polymer are particularly applicable in the field of solid propellant compositions where the improved properties are extremely beneficial.
- the following examples illustrate the manufacture of solid propellants utilizing the modified binders of this invention, and the improved properties obtained therefrom.
- Example 11 A propellant composition utilizing a modified telechelic polybutadiene polymer was manufactured. Into a two and one-half Baker-Perkins propellant mixer was carefully weighed 426.48 grams (17.77 weight percent) of modified telechelic carboxy-terminated polybutadiene. The polybutadiene was modified with vinylcyclohexene as described in Example I. Additionally weighed into the mixer was 384 grams (16.00 weight percent) of finelypowdered aluminum metal which acts as the fuel. The mixer was then turned on to disperse the aluminum in the liquid binder material. During this process a vacuum was applied to the mixer.
- Example IV To illustrate the improved properties obtained with the novel polymeric binders of this invention, tests were run comparing the propellant compositions prepared according to Examples II and III with a control propellant which had the following compositions:
- e is the elongation at maximum tensile strength, expressed in percent; S is the maximum tensile strength in p.s.i.; and E is the tangent modulus of elasticity.
- All test specimens were standard JANAF dogbones. All testing was done on an Instron machine at a strain rate of 0.77 in.-in. min.
- the propellant elongation increased from an average of about 30 percent for the control propellant over the entire range of temperatures to an average exceeding 50 percent for the propellant utilizing the modified binder of this invention.
- the percent elongation nearly doubled utilizing the concepts set forth herein.
Landscapes
- Chemical & Material Sciences (AREA)
- Health & Medical Sciences (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Medicinal Chemistry (AREA)
- Polymers & Plastics (AREA)
- Life Sciences & Earth Sciences (AREA)
- Dispersion Chemistry (AREA)
- Molecular Biology (AREA)
- Crystallography & Structural Chemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Addition Polymer Or Copolymer, Post-Treatments, Or Chemical Modifications (AREA)
Description
United States Patent 3,305,523 MODIFICATION OF TELECHELIC-TYPE POLYMERS Charles II. Burnside, Waco, Tex., assignor to North American Aviation, Inc. No Drawing. Filed Aug. 30, 1962, Ser. No. 221,654 4 Claims. (Cl. 26046.5)
This invention concerns a novel solid propellant polymeric binder. More specifically, this invention pertains to a solid propellant binder having unexpectedly high elongation properties and high solid loading ability.
A typical composite solid propellant is comprised of solid particulate fuel such as minute particles of a metal and a solid particulate oxidizer which serves to oxidize the fuel particles. In order to secure the particles of oxidizer and fuel in an intimate mixture necessary for effective combustion and practical use, a resinous matrix material or binder is required. The binder material normally additionally serves as a fuel component of the solid propellant. This binder is normally a liquid resinous i material and when mixed with high percentages of the solid particles of fuel and oxidizer, forms a viscous material which may be cast in a mold and cured for the desired shaped propellant charge. Physical properties are desired in a solid propellant. These properties are normally in an interrelated combination in that the maximum dilute of all the parameters does not necessarily yield the best solid propellant. One parameter depends upon the value of another in several performance evaluations. The solid propellant should be stable for a long period of time and should not deteriorate chemically or physically during storage. High density of the solid propellant permits the use of a small chamber volume and therefore small chamber weight. The propellant should lend itself readily to production and have desirable fabrication properties such as adequate fluidity during casting or easy to control chemical processes such as curing and a minimal volume change after casting or molding. The mechanical properties and the combustion characteristics such as burning rate should be predictable and uneifected appreciably over a wide range of storage and operating temperatures. This means that the temperature sensitivity should be low.
Additionally the propellant should exhibit good mechanical properties, particularly its tensile, compressive and sheer strength and its rnodulous of elasticity and elongation. Finally the propellant should have high solids loading capability.
The previously set forth desirous properties in a solid propellant have been accomplished through the use of propellants which utilize a carboxy-terminated linear polybutadiene binder. The so-called Flexadyne family of solid propellants was developed specifically to have superior mechanical properties in tension, compression, tear and creep and to maintain a good balance of such properties over the temperature range 75 to 170 F.
One of the components of this family of propellants that gives the group the outstanding properties is the propellant binder polymer utilized. The polymer binder used in these propellants is a carboxy-terminated linear polybutadiene. The excellent properties of the binder are attained when the starting initial molecules of butadiene have the hydrogen atoms at the double bonds in carefully ordered positions in space to obtain a symmetrical cross-linking of the cured polymer. Additionally, the polymer has a properly controlled cistrans stereoisomerism, when the polymerization is stopped at 100 molecules of butadiene per chain, when the number or nature of possible side chains is concerned and when a carboxylic group is attached at either end of each polybutadiene molecule and nowhere else. The resulting symmetrical 3,305,523 Patented Feb. 21, 1967 structure has good elastorneric properties and is achieved in the binder by controlling the chemistry and of the polymerization process itself. This type of polybutadiene polymer is referred to as a telechelic-type polymer and the method of preparation is well known in the art and is described in the Journal of Polymer Science, vol. XLVI, Issue 148, pp. 535-539 (1960). An example of the carboxy-terminated polybutadiene binder used in this group of propellants is Butarez CTL manufactured by the Phillips Petroleum Company. In addition to the carboxy-terminated linear polybutadiene telechelic-type polymers other possible terminal groups can successfully be utilized in the present applications. Such other terminal functional groups would include hydroxy radicals, amine, mercapto and isocyanate radicals. It is understood that any telechelic polymer regardless of the terminal functional groups can be successfully utilized.
The present invention concerns the further improvement of mechanical properties of the telechelic polymer binders previously described. Particularly, the invention is directed to the improvement of the mechanical properties of the binder material over a wide range of temperature varying from less than -70 F. to excess of F. The greatly improved mechanical properties are accomplished in the present invention by the extension of the telechelic polymer chains through increasing the chain length and molecular Weight by the addition of from 0.4 to 10 parts by weight of difunctional materials, such as, for example, vinylcyclohexene dioxide. Particularly preferred is from 0.6 to 5 parts by weight of the difunctional additives. The difunctional additive that is utilized depends upon the functional terminal group in the telechelic polymer compound. The difunctional additive must be one that will react with the functional terminal group of the polymer in order for an effective result to be obtained. As will hereinafter be set forth, various difunctional additives may be used depending upon the functional terminal group of the telechelic polymer. Thus, as can be seen, the difunctional additive becomes part of the polymer chains.
constancy of mechanical properties of a solid propellant or erratic temperature change is desirable so that brittleness at low temperature and plastic flow at high temperatures do not limit the use of the rocket propellant to a narrow temperature range. One of the many requirements of a propellant charge is that it be plastic enough or have enough elongation to change dimensions without cracking as required by the rocket motor expansion under pressure. High elongation of the rocket propellant is desirable to accommodate the differential expansion properties between the motor chamber and the propellant. As a result, it is of great significance that the mechanical properties of a solid propellant binder of a telechelic-type can be greatly improved through the addition of the difunctional compounds of this invention. The elongation of the propellants utilizing the binders of this invention have increased 40 to 50 percent over a temperature range of 70 to 170 F. In some instances this represents a doubling of the percent elongation of the propellant.
The telechelic polymers used in the propellant binder as previously described are not only polybutadienes. The invention also pertains to the improvement of the mechanical properties of telechelic polymers which may be of other skeletal structures such as any polymerizable monomer containing an ethylenic linkage.
Non-limiting examples of the monomers that may be utilized in the invention to produce the telechelic polymers include the vinyl halides such as iodoethene, bromoethene, fiuorethene, chloroethene; vinylidene halides including vinylidene chloride, vinylidene iodide, and the like; vinyl esters of carboxylic acids having 1 to 10 carbon atoms including vinyl acetate and the like; and N-substituted acrylamides and methyacrylamide including N methylacrylamide, N-propyl methyacrylamide, N-hexyl aerylamide and the like; allyl and methya-llyl monomers including allylamine, N-methylallylamine, allyl bromide, allyl alcohol, allyl chloride, allyl cyanide, allyl fluoride, allyl glycidyl ether, allyl isodide, allyl mercaptan, allyl sulphide, and the like; isopropenyl monomers including isopropenyl bromide, isopropenyl chloride, isopropenyl fluoride, and the like; vinyl compounds including vinyl alcohol, vinyl bromide, vinyl fluoride, vinyl cyanide, vinyl sulphide, vinyl tribromide, vinyl ether, vinyl napthalene, and the like; vinyl ethers including ethenylenyethene, propenyloxyethene, and the like; acrylates and methacrylates including ethyl acrylate, methyl acrylates, propyl methacrylates, hydroxy propyl methacrylate, hexyl acrylate, and the like; glycidyl acrylates, .glycidyl methacrylates, and the like; and styrene. Additionally, mixtures of the above monomers could be used. For example, the copolymer of butadiene and styrene is applicable.
The functional terminal groups that are present can be selected from hydroxy, amino, mercapto and isocyanate radicals, in addition to any other reactive functional groups. As previously described, the compounds which are added to the telechelic polymer to improve the mechanical properties of the propellants formed can be varied depending upon the functional terminal groups present in the telechelic polymer. When one of the functional terminal groups of the telechelic polymer is a carboxy radical, the difunctional additives may include dialcohols such as dihydroxybenzene, dihydroxynapthaline, dihydroxybutane, and the like; diepoxides such as vinylcyclohexene dioxide, the Epon resins which are the products of epichlorohydrin and bis-phenol-A, diamines such as ethylene diamine, butylene diamine, hexamethylene diamine and the like; diamines such as hydrazine and the like; and lbis-chlorocarbonates such as ethylene bis-chlorocarbonate and the like.
When the functional telechelic groups in the telechelic polymers are hydroxy radicals, the difunctional additives may be selected from the group consisting of diimines; dicarboxylic acid chlorides such as succinyl chloride and the like; dicarboxylic acids such as maleic acid and the like; phosgene; bis-chlocarbonates and the like; and diisocyanates which are formed by treating diamines such as toluene 2,4-diamine, hexamethy aminediamine, and the like with phosgene.
When the functional telechelic groups in the telechelic polyers are amino groups, the difunctional additives may be selected from the group consisting of dicarboxylic acids; diamines; diepoxides; and dialdahydes such as malonic aldehyde and succinic aldehyde.
When the telechelic polymers have terminal functional groups that are mercaptans, the difunctional additives utilized may be acid chlorides; bischlorocarbonates; and usually any compound containing two double bonds (diolefins) capable of reacting with the mercaptan, such as ethyleneglycol diacrylate, for example. It is believed the invention will be further understood from the following detailed examples.
When the telechelic polymers have terminal functional groups that are isocyanates, the terminal difunctional additives having difunctional terminal hydroxy may be any compounds or amino groups or one of each functional type.
Example 1 Into a two and one fourth gallon Baker-Perkins dispersion blade mixer was added 1000 grams of Butarez CTL which is a carboxy-terminated linear polybutadiene. Additionally added was 6 grams of vinylcyclohexenedioxide. Water, at 165 F., was circulated through the mixer heating jacket. The material was then blended for fifteen minutes. A 28-inch vacuum was then applied and mixing continued for an additional ten minutes to remove the air present. The contents of the mixer were then poured into a large polyethylene bag. The bag was then sealed and then placed in a metal bucket container, the bag serving two functions. (1) To prevent contact with metal surfaces and (2) to prevent contact with air. The material was then heated for 168 hours at 170 F. A liquid modified polymer of this invention was obtained upon cooling of the material at room temperature and the removal from the sealed bag. The above procedure was repeated utilizing 1000 grams of the Butarez CTL and 10 grams of 1,3-bis[3 (2,3-epoxy-propoxy)propyl]tetra methyl disiloxane. A modified telechelic polymer of this .invention was obtained.
As is in the reaction of most polymeric-type materials, the temperature and length of time of reaction varies considerably. The temperature of reaction may vary from, for example, 15 0 F. to 225 F. with the time of reaction varying according to the temperature utilized with the higher temperatures requiring less reaction time. Thus, reaction times can vary from 145 hours to hours. Basically more important than the temperature and time of reaction ,is the assurance of conversion to the desired product. During the reaction of the difunctional groups with the telechelic polymers, samples of the mixture are taken from time to time during the reaction period. The samples are analyzed, for example, in the case of the carboxy-terminated telechelic polymers to determine the ephr value, that is the carboxyl equivalents. Once the carboxyl equivalents of the mixtures stabilize, there is an indication that the reaction has gone to completion and all of the difunctional groups that are 'going to react have reacted with the carboxy groups present. At this time the reaction is stopped. The same process could be taken when, for example, mercaptan groups are the terminal functional groups of the telechelic polymer. Mercaptan equivalents would be determined during the course of the reaction until a stabilized condition is reached at which time the reaction has gone to completeion and can be stopped.
The invention has peculiar applicability to the field of solid propellants wherein the polymers are used as binders to secure the solid particulate matter utilized.
The solid material which may be dispersed throughout the polymer matrix is usually in finely divided form having a particle size ranging from about 1-500 microns or greater in diameter. When the composition is intended as a solid propellant grain, it is often desirable to employ a combination of two or more different particle size ranges. For example, solid propellants are prepared in which the finer material comprises a fine particle size range of from 1 to about 75 microns and a coarse range of from about 75 to 500. However, particles of any size within the range of 1500 microns may be employed without regard to particle size. This gives desirable burning rates to the propellant. The particle size ranges may be adjusted depending upon the particular binder-fueloxidizer combination employed and the specific impulse desired.
The solid substances with which the polymeric materials are loaded may be inert pigments such as titanium dioxide, lead oxide, ferric oxide, carbon black, powdered metals and alloys, metal fluorides, asbestos fibers, etc.
When the solids are oxidizing agents, they can be compounds such as metal perchlorates and metal nitrates. The metal perchlorates employed as oxidizing agents or oxygen carriers in the compositions are anhydrous and have the general formula M(ClO wherein M is NH or a metal and x is the valence of M. Since the propellant composition is required to withstand high temperature storage, it is preferable that the melting point and the decomposition temperature of the oxidizer be as high as possible. The perchlorates of the Group I-A, Group- I-B, and Group II-A metals are found to have the re-- quired high temperature stability and are employed in the preparation of propellant compositions by the process of this invention. Hence, the metal perchlorates used in the preparation of the propellant compositions include lithium perchlorate, sodium perchlorate, potassium perchlorate, rubidium perchlorate, and cesium perchlorate which are the perchlorates of the metals of Group I-A of the Periodic Table of Elements; silver perchlorate which is a perchlorate of the Group IB metal; and magnesium perchlorate, calcium perchlorate, strontium perchlorate, and barium perchlorate which are the perchlorates of the Group II-A metals. In addition to the metal perchlorates, the compound ammonium perchlorate finds extensive use in propellant compositions. Examples of the nitrates of the Group IA, and I-B and II-B which are employed in preparing propellant compositions by the process of this invention are compounds such as lithium nitrate, sodium nitrate, potassium nitrate, magnesium nitrate, calcium nitrate, barium nitrate, strontium nitrate, etc; Ammonium nitrate is also used.
The ratio of total solids-to-polymeric binder material in a propellant falls in the range of from about 1:1 to about 9:1 with an optimum ratio of about 85:15.
Other substances which are employed in the preparation of propellants by the process of this invention include minor amounts of burning catalysts, well known in propellant compositions. These are composed of one or a mixture of two or more metal oxide powders in amounts suificient to improve the burning rate of the composition. The amounts usually range from about 0.01 to about 3 weight percent, based on the weight of the oxidizer employed. The particle size of the powders can range from about 10 to about 250 microns in diameter. Non-limiting examples of metals that serve as burning catalysts are copper, vanadium, chromium, silver, molybdenum, sinconium, antimony, manganese, iron, cobalt, and nickel. Examples of metal oxide burning catalysts are ferric oxide, aluminum, copper oxide, chromic oxide, as well as the oxides of the other metals mentioned above.
The fuel particles that are employed in a solid propellant grain are usually a metal or a metal alloy, preferably the fuel contains 1 or more metals of groups I-A, II-A, III-A and groups I-B through VII-B, group III of the Periodic Table. Thus, the metals may contain group I-A elements such as lithium and group IIA metals such as beryllium or magnesium. Illustrative of the group III-A metals is aluminum. The metals of groups I-B through VII-B include copper, silver, zinc, manganese, iron, nickel, platinum and the like. Particularly preferred for inclusion in the polymer matrix are aluminum, beryllium and lithium since these metals are of relatively low molecular weight giving low molecular weight combustion products in addition to having high heats of combustion.
Burning rate depressants and modifiers are also sometimes advantageously added to the solid propellant grain of this invention. These are generally compounds which tend to inhibit burning reaction rates or absorb heat and include specifically carbonyl chloride, oximide, nitroguanidine, guanidine nitrate, and oxalic acid.
As previously described, the improved properties obtained by the modification of a telechelic polymer are particularly applicable in the field of solid propellant compositions where the improved properties are extremely beneficial. The following examples illustrate the manufacture of solid propellants utilizing the modified binders of this invention, and the improved properties obtained therefrom.
Example 11 A propellant composition utilizing a modified telechelic polybutadiene polymer was manufactured. Into a two and one-half Baker-Perkins propellant mixer was carefully weighed 426.48 grams (17.77 weight percent) of modified telechelic carboxy-terminated polybutadiene. The polybutadiene was modified with vinylcyclohexene as described in Example I. Additionally weighed into the mixer was 384 grams (16.00 weight percent) of finelypowdered aluminum metal which acts as the fuel. The mixer was then turned on to disperse the aluminum in the liquid binder material. During this process a vacuum was applied to the mixer. After the aluminum had been dispersed within the binder material, 1584 grams (66.00 weight percent) of the oxidizer which was ammonium perchlorate was weighed and added to the mixer which was then turned on for a short period, approximately two or three minutes to disperse the oxidizer. The vacuum was then applied and mixing was continued until the constituents therein reached the temperature of l60170 F. at which time the mixing was stopped. The temperature is reached due to the circulating of a heating fluid in the jacket that surrounds the mixer. After the mixing had stopped and the cure temperature had been reached,
5.52 grams (.23 weight percent) of a curative which was MAPO (tris[l-(2-methyl)-aziridinyl]phosphine oxide) was added to the mixed constituents without any vacuum being applied. The mixer was then turned on to disperse the curative within the mixture. After the curative had been dispersed, the contents were then poured into a pan 8 by 8 inches and 3 inches deep and cast at a cure temperature of 170 for 48 hours. The curing time can vary and often the mixture is cured at 96 hours at 150 F., it being understood that the cure time decreases with increase in temperature. The resultant solid propellant having the modified carboxy-terminated polybutadiene polymer was obtained. The propellant was then stamped out in the JANAF dogbone configuration for use in determining its physical properties.
Example Ill Grams Wt.
Percent Garb cry-terminated linearrpolybutadiene modified with l,3-bis[3(2,3epoxyproxy)propyl] tetra methyl disiloxaue 445 17. 8 Ammonium perchlorate, 1, 650 66. 0 Aluminum 10. 0 MAPO 5 20 A propellant composition utilizing a modified polybutadiene binder was obtained.
Example IV To illustrate the improved properties obtained with the novel polymeric binders of this invention, tests were run comparing the propellant compositions prepared according to Examples II and III with a control propellant which had the following compositions:
Percent by weight Linear carboxy-terminated polybutadiene (unmodified teleohelic polymer) l8 Ammonium perchlorate 66 Aluminum 16 The results obtained are set forth in Table I.
TABLE I Test Temp Control Example I Example II Deg. F
em, percent 26 48 51 S..., p.s.i
so 88 89 E, .s.i 455 275 255 cm, percent 34 G2 G6 Sm, p.s.i- 124 E..., psi. 5 10 345 330 em, percent- 32 51 51 m. p.s.i- 247 241 235 E,.., p.s.i 2, 010 1, 660 2,020
In Table I, e is the elongation at maximum tensile strength, expressed in percent; S is the maximum tensile strength in p.s.i.; and E is the tangent modulus of elasticity. All test specimens were standard JANAF dogbones. All testing was done on an Instron machine at a strain rate of 0.77 in.-in. min. Of considerable import is the fact that the propellant elongation increased from an average of about 30 percent for the control propellant over the entire range of temperatures to an average exceeding 50 percent for the propellant utilizing the modified binder of this invention. As can readily be seen from the table, the percent elongation nearly doubled utilizing the concepts set forth herein. Additionally, as can be seen from the table, the maximum tensile strength increased except for a slight decrease at 70. This is a significant aspect of the effect of the present invention, since the elasticity of the propellant can now be greatly increased without any detrimental affect on the maximum tensile strength. A'sign'ificant advance of the art has been accomplished in providing a propellant binder that will provide superior and improved physical properties over an extreme range of temperatures as seen in Table I.
Although the invention has been described and illustrated in detail, it is to be clearly understood that the same is by way of illustration and example only and is not to be taken by way of limitation, the spirit and scope of this invention being limited only by the terms of the appended claims.
I claim:
1. The compound obtained by the reaction of carboxyterminated polybutadiene and 1,3-bis [3(2,3-epoXy-propoxy)propyl] tetra methyl disiloxane.
References Cited by the Examiner UNITED STATES PATENTS 2,848,442 8/1958 Svetlik 260-82.1 3,053,708 9/1962 Hall et al. 149-19 3,055,781 9/1962 Yamamoto 14919 3,070,583 12/1962 Uraneck 26082.1 3,087,844 4/1963 Hudson et al. 14919 3,147,161 9/1964 Abere et a1 14919 FOREIGN PATENTS 226,634 4/ 1959 Australia.
LEON I. BERCOVITZ, Primary Examiner. REUBEN EPSTEIN, C. D. QUARFORTH, Examiners.
L. A. SEBASTIAN, B. R. PADGETT,
Assistant Examiners.
Claims (2)
1. THE COMPOUND OBTAINED BY THE REACTION OF CARBOXYTERMINATED POLYBUTADIENE AND 1, 3-BIS (3, (2, 3-EXPOXY-PROPOXY) PROPYL) TETRA METHYL DISILOXANE.
3. THE METHOD OF IMPROVING THE PHYSICAL STRENGTH PROPERTIES OF CARBOXY-TERMINATED POLYBUTADIENE WHICH COMPRISES REACTING SAID POLYBUTADIENE WITH 1, 3-BIS (3(2, 3EPOXY-PROPOXY) PROPYL) TETRA METHYL DISILOXANE.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US221654A US3305523A (en) | 1962-08-30 | 1962-08-30 | Modification of telechelic-type polymers |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US221654A US3305523A (en) | 1962-08-30 | 1962-08-30 | Modification of telechelic-type polymers |
DEN0029345 | 1966-10-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3305523A true US3305523A (en) | 1967-02-21 |
Family
ID=25989059
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US221654A Expired - Lifetime US3305523A (en) | 1962-08-30 | 1962-08-30 | Modification of telechelic-type polymers |
Country Status (1)
Country | Link |
---|---|
US (1) | US3305523A (en) |
Cited By (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3418184A (en) * | 1968-01-16 | 1968-12-24 | Navy Usa | Smoke producing propellant |
US3433158A (en) * | 1966-02-10 | 1969-03-18 | Us Army | Solid propellant grain with surface bonded burning inhibitor composition of hydroxy-terminated polybutadiene |
US3434990A (en) * | 1966-05-13 | 1969-03-25 | Us Navy | Accelerating the cure rate of carboxylated polybutadiene-aziridinyl compound mixtures with lithium oleate |
US3462516A (en) * | 1964-08-31 | 1969-08-19 | Phillips Petroleum Co | Blends of a liquid diene polymer and maleic anhydride copolymer |
US3472826A (en) * | 1968-05-23 | 1969-10-14 | Union Carbide Corp | Saturated hydrocarbon prepolymer and reaction products thereof |
US3476622A (en) * | 1966-12-20 | 1969-11-04 | Asahi Chemical Ind | Carboxy-terminated composite rocket propellant and process for producing using an amide additive |
US3498855A (en) * | 1967-07-24 | 1970-03-03 | Standard Oil Co | Ammonium nitrate propellant compositions containing thermoplastic polymeric resins |
US3498856A (en) * | 1967-07-24 | 1970-03-03 | Standard Oil Co | Combustion catalyst for solid ammonium nitrate propellant grain |
US3501357A (en) * | 1967-04-12 | 1970-03-17 | Asahi Chemical Ind | Composite propellants containing block copolymers |
US3507114A (en) * | 1967-11-27 | 1970-04-21 | Webb James E | Solid propellant liner |
US3507721A (en) * | 1967-08-01 | 1970-04-21 | United Aircraft Corp | Crosslinked carboxy-terminated polyether propellant compositions containing nitrato esters |
US3658608A (en) * | 1970-09-23 | 1972-04-25 | Nasa | Hydrazinium nitroformate propellant stabilized with nitroguanidine |
US3698191A (en) * | 1967-08-01 | 1972-10-17 | United Aircraft Corp | Nonsustaining hybrid propellant grain |
US3790416A (en) * | 1970-07-22 | 1974-02-05 | Hercules Inc | Composite propellant including (u) polyfunctional amine |
FR2213295A1 (en) * | 1973-01-04 | 1974-08-02 | Goodrich Co B F | Phenolic terminated elastomers - from carboxy terminated diene elastomers for impact modifying resins |
US3853646A (en) * | 1967-04-05 | 1974-12-10 | Rockwell International Corp | Smokeless composite propellants containing carboxy - or hydroxy - terminated polymers and a nitro-organic oxidizer |
US3867354A (en) * | 1968-08-15 | 1975-02-18 | Mini Of Technology | Chromium salicylate catalyzed epoxide-carboxylic acid esterification |
US3890173A (en) * | 1968-11-29 | 1975-06-17 | Dow Chemical Co | Solid propellant containing ethylene-carboxylic acid polymers cured with azeridine-based resins |
US3948698A (en) * | 1967-09-06 | 1976-04-06 | Hercules Incorporated | Solid propellant compositions having epoxy cured, carboxy-terminated rubber binder |
US3957551A (en) * | 1971-12-17 | 1976-05-18 | The Dow Chemical Company | Propellant compositions having carboxyl containing binder cured with a glycidyl thioether |
US3982975A (en) * | 1967-09-06 | 1976-09-28 | Hercules Incorporated | Propellants having improved resistance to oxidative hardening |
US3984265A (en) * | 1967-09-06 | 1976-10-05 | Hercules Incorporated | Composite propellants having improved resistance to thermal oxidation |
US4019933A (en) * | 1973-07-27 | 1977-04-26 | The United States Of America As Represented By The Secretary Of The Army | Pot life extension of isocyanate cured propellants by aziridine compounds |
US4050968A (en) * | 1970-04-29 | 1977-09-27 | The United States Of America As Represented By The Secretary Of The Navy | Explosive composition containing a hydroxyalkyl acrylate copolymer binder |
US4057441A (en) * | 1976-03-29 | 1977-11-08 | Thiokol Corporation | Solid propellant with burning rate catalyst |
US4108696A (en) * | 1968-04-01 | 1978-08-22 | Thiokol Corporation | Solid propellant having incorporated therein a ferrocene combustion catalyst |
US4111729A (en) * | 1969-08-05 | 1978-09-05 | Paine T O Administrator Of The | Inhibited solid propellant composition containing beryllium hydride |
DE2854260A1 (en) * | 1978-01-04 | 1979-07-12 | Hercules Inc | PHOTOPOLYMERIZABLE MIXTURES FOR PRINTING PLATES |
US4168362A (en) * | 1974-11-25 | 1979-09-18 | The United States Of America As Represented By The Secretary Of The Navy | Non-migrating ferrocene containing solid propellant binder |
US4241661A (en) * | 1967-09-06 | 1980-12-30 | Hercules Incorporated | Composite propellant with surface having improved strain capacity |
US4315830A (en) * | 1972-01-19 | 1982-02-16 | The United States Of America As Represented By The Secretary Of The Navy | Method for altering the characteristics of polymers |
US4318270A (en) * | 1968-04-11 | 1982-03-09 | The United States Of America As Represented By The Secretary Of The Navy | Additives for suppressing the radar attenuation of rocket propellant exhaust plumes |
US4337103A (en) * | 1967-09-06 | 1982-06-29 | Hercules Incorporated | Composite propellant with differentially cured area at initial burn surface |
US4366010A (en) * | 1978-09-21 | 1982-12-28 | Sedat Georges A | Smoke-producing pyrotechnic composition and its application |
US4518677A (en) * | 1978-01-04 | 1985-05-21 | Hercules Incorporated | Process for making printing plates |
WO1990008166A1 (en) * | 1989-01-17 | 1990-07-26 | Ceska Gary W | Thermoplastic elastomer composed of macromolecular monomers and alkoxyalkyl acrylate monomers |
US4959419A (en) * | 1986-12-20 | 1990-09-25 | Bayer Aktiengesellschaft | Polymeric emulsifiers based on aminotelechelic oligomers I |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2848442A (en) * | 1955-04-11 | 1958-08-19 | Phillips Petroleum Co | Oil resistant conjugated diene-heterocyclic nitrogen base copolymers |
US3053708A (en) * | 1959-02-12 | 1962-09-11 | Phillips Petroleum Co | High impulse solid propellant composition |
US3055781A (en) * | 1957-11-28 | 1962-09-25 | Yamamoto Akira | Composite propellants |
US3070583A (en) * | 1954-01-04 | 1962-12-25 | Phillips Petroleum Co | Method for solubilizing an acidic copolymer, and water-soluble product obtained thereby |
US3087844A (en) * | 1959-07-24 | 1963-04-30 | Phillips Petroleum Co | Solid composite propellants containing aziridinyl curing agents |
US3147161A (en) * | 1961-06-19 | 1964-09-01 | Minnesota Mining & Mfg | Propellant composition cured with aziridinyl compounds |
-
1962
- 1962-08-30 US US221654A patent/US3305523A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3070583A (en) * | 1954-01-04 | 1962-12-25 | Phillips Petroleum Co | Method for solubilizing an acidic copolymer, and water-soluble product obtained thereby |
US2848442A (en) * | 1955-04-11 | 1958-08-19 | Phillips Petroleum Co | Oil resistant conjugated diene-heterocyclic nitrogen base copolymers |
US3055781A (en) * | 1957-11-28 | 1962-09-25 | Yamamoto Akira | Composite propellants |
US3053708A (en) * | 1959-02-12 | 1962-09-11 | Phillips Petroleum Co | High impulse solid propellant composition |
US3087844A (en) * | 1959-07-24 | 1963-04-30 | Phillips Petroleum Co | Solid composite propellants containing aziridinyl curing agents |
US3147161A (en) * | 1961-06-19 | 1964-09-01 | Minnesota Mining & Mfg | Propellant composition cured with aziridinyl compounds |
Cited By (38)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3462516A (en) * | 1964-08-31 | 1969-08-19 | Phillips Petroleum Co | Blends of a liquid diene polymer and maleic anhydride copolymer |
US3433158A (en) * | 1966-02-10 | 1969-03-18 | Us Army | Solid propellant grain with surface bonded burning inhibitor composition of hydroxy-terminated polybutadiene |
US3434990A (en) * | 1966-05-13 | 1969-03-25 | Us Navy | Accelerating the cure rate of carboxylated polybutadiene-aziridinyl compound mixtures with lithium oleate |
US3476622A (en) * | 1966-12-20 | 1969-11-04 | Asahi Chemical Ind | Carboxy-terminated composite rocket propellant and process for producing using an amide additive |
US3853646A (en) * | 1967-04-05 | 1974-12-10 | Rockwell International Corp | Smokeless composite propellants containing carboxy - or hydroxy - terminated polymers and a nitro-organic oxidizer |
US3501357A (en) * | 1967-04-12 | 1970-03-17 | Asahi Chemical Ind | Composite propellants containing block copolymers |
US3498855A (en) * | 1967-07-24 | 1970-03-03 | Standard Oil Co | Ammonium nitrate propellant compositions containing thermoplastic polymeric resins |
US3498856A (en) * | 1967-07-24 | 1970-03-03 | Standard Oil Co | Combustion catalyst for solid ammonium nitrate propellant grain |
US3507721A (en) * | 1967-08-01 | 1970-04-21 | United Aircraft Corp | Crosslinked carboxy-terminated polyether propellant compositions containing nitrato esters |
US3698191A (en) * | 1967-08-01 | 1972-10-17 | United Aircraft Corp | Nonsustaining hybrid propellant grain |
US4337103A (en) * | 1967-09-06 | 1982-06-29 | Hercules Incorporated | Composite propellant with differentially cured area at initial burn surface |
US4241661A (en) * | 1967-09-06 | 1980-12-30 | Hercules Incorporated | Composite propellant with surface having improved strain capacity |
US3984265A (en) * | 1967-09-06 | 1976-10-05 | Hercules Incorporated | Composite propellants having improved resistance to thermal oxidation |
US3982975A (en) * | 1967-09-06 | 1976-09-28 | Hercules Incorporated | Propellants having improved resistance to oxidative hardening |
US3948698A (en) * | 1967-09-06 | 1976-04-06 | Hercules Incorporated | Solid propellant compositions having epoxy cured, carboxy-terminated rubber binder |
US3507114A (en) * | 1967-11-27 | 1970-04-21 | Webb James E | Solid propellant liner |
US3418184A (en) * | 1968-01-16 | 1968-12-24 | Navy Usa | Smoke producing propellant |
US4108696A (en) * | 1968-04-01 | 1978-08-22 | Thiokol Corporation | Solid propellant having incorporated therein a ferrocene combustion catalyst |
US4318270A (en) * | 1968-04-11 | 1982-03-09 | The United States Of America As Represented By The Secretary Of The Navy | Additives for suppressing the radar attenuation of rocket propellant exhaust plumes |
US3472826A (en) * | 1968-05-23 | 1969-10-14 | Union Carbide Corp | Saturated hydrocarbon prepolymer and reaction products thereof |
US3867354A (en) * | 1968-08-15 | 1975-02-18 | Mini Of Technology | Chromium salicylate catalyzed epoxide-carboxylic acid esterification |
US3890173A (en) * | 1968-11-29 | 1975-06-17 | Dow Chemical Co | Solid propellant containing ethylene-carboxylic acid polymers cured with azeridine-based resins |
US4111729A (en) * | 1969-08-05 | 1978-09-05 | Paine T O Administrator Of The | Inhibited solid propellant composition containing beryllium hydride |
US4050968A (en) * | 1970-04-29 | 1977-09-27 | The United States Of America As Represented By The Secretary Of The Navy | Explosive composition containing a hydroxyalkyl acrylate copolymer binder |
US3790416A (en) * | 1970-07-22 | 1974-02-05 | Hercules Inc | Composite propellant including (u) polyfunctional amine |
US3658608A (en) * | 1970-09-23 | 1972-04-25 | Nasa | Hydrazinium nitroformate propellant stabilized with nitroguanidine |
US3957551A (en) * | 1971-12-17 | 1976-05-18 | The Dow Chemical Company | Propellant compositions having carboxyl containing binder cured with a glycidyl thioether |
US4315830A (en) * | 1972-01-19 | 1982-02-16 | The United States Of America As Represented By The Secretary Of The Navy | Method for altering the characteristics of polymers |
FR2213295A1 (en) * | 1973-01-04 | 1974-08-02 | Goodrich Co B F | Phenolic terminated elastomers - from carboxy terminated diene elastomers for impact modifying resins |
US4019933A (en) * | 1973-07-27 | 1977-04-26 | The United States Of America As Represented By The Secretary Of The Army | Pot life extension of isocyanate cured propellants by aziridine compounds |
US4168362A (en) * | 1974-11-25 | 1979-09-18 | The United States Of America As Represented By The Secretary Of The Navy | Non-migrating ferrocene containing solid propellant binder |
US4057441A (en) * | 1976-03-29 | 1977-11-08 | Thiokol Corporation | Solid propellant with burning rate catalyst |
DE2854260A1 (en) * | 1978-01-04 | 1979-07-12 | Hercules Inc | PHOTOPOLYMERIZABLE MIXTURES FOR PRINTING PLATES |
US4442302A (en) * | 1978-01-04 | 1984-04-10 | Hercules Incorporated | Photopolymer compositions for printing plates |
US4518677A (en) * | 1978-01-04 | 1985-05-21 | Hercules Incorporated | Process for making printing plates |
US4366010A (en) * | 1978-09-21 | 1982-12-28 | Sedat Georges A | Smoke-producing pyrotechnic composition and its application |
US4959419A (en) * | 1986-12-20 | 1990-09-25 | Bayer Aktiengesellschaft | Polymeric emulsifiers based on aminotelechelic oligomers I |
WO1990008166A1 (en) * | 1989-01-17 | 1990-07-26 | Ceska Gary W | Thermoplastic elastomer composed of macromolecular monomers and alkoxyalkyl acrylate monomers |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3305523A (en) | Modification of telechelic-type polymers | |
US3035948A (en) | Gelled nitroalkane propellants | |
US3002830A (en) | Method of manufacturing solid propellants having a polymeric fuel-binder using a plurality of crosslinking agents | |
US4915755A (en) | Filler reinforcement of polyurethane binder using a neutral polymeric bonding agent | |
US3255059A (en) | Fluoroalkyl acrylate polymeric propellant compositions | |
WO2020212785A1 (en) | Composite propellant manufacturing process based on deposition and light-activated polymerization for solid rocket motors | |
US3255281A (en) | Propellant casting method | |
US5472532A (en) | Ambient temperature mix, cast, and cure composite propellant formulations | |
US3647891A (en) | Methylol-terminated fluorocarbon polymers | |
US3745074A (en) | Composite solid propellant with additive to improve the mechanical properties thereof | |
US3748199A (en) | Composite propellants containing hydroxylammonium perchlorate | |
CA1056984A (en) | Curable binding systems | |
US3649389A (en) | Polymeric propellant and liner composition using a trimer acid | |
US3627596A (en) | Solid propellant employing a polymer containing a carboranyl group | |
US3265543A (en) | Composite propellant containing nitroglycerin | |
EP3137440B1 (en) | Bonding agents for nitrogen-containing oxidizers | |
US3087843A (en) | Solid propellant compositions | |
US3589954A (en) | Novel epoxy cured polymer binders and propellant compositions prepared therewith | |
US3698967A (en) | Method of curing propellants containing carboxyl terminated polyalkadienes using an organic iron salt | |
US6197135B1 (en) | Enhanced energetic composites | |
US3880683A (en) | Castable high explosive of cyclotetramethylenetetranitramine and dodecenyl succinic anhydride-vinyl cyclohexene dioxide polymer binder | |
US3830674A (en) | Propellant composition containing beryllium and an energetic difluoramino containing binder | |
US3499289A (en) | Monopropellant in binder matrix | |
US3957551A (en) | Propellant compositions having carboxyl containing binder cured with a glycidyl thioether | |
US3725152A (en) | Polymeric binders for use in hybrid rocket propellents |