Elastomeric rocket motor insulation
A rocket motor insulation including an elastomer-based polymer is improved in its processability by the addition of silica particles treated with a hydrophobic coating. The insulation also preferably includes a metallic coagent cross-linker, which when used in combination with the hydrophobic silica particles increases the tear strength and the elasticity of the insulation, while at the same time not adversely affecting the bonding characteristics of the insulation.
1. An elastomeric rocket motor insulation comprising, in a precured state, at least the following ingredients:
at least one organic polymer curable into an elastomer;
at least one peroxide curative;
at least one curative coagent comprising a polyfunctional metal salt for forming organometallic cross-link bonds; and
a filler comprising at least one member selected from the group consisting of silica particles and silicate particles, the filler being treated with at least one hydrophobic surface agent.
2. The elastomeric rocket motor insulation of claim 1 , wherein the elastomer comprises at least one member selected from the group consisting of ethylene-propylene-diene monomer (EPDM) rubbers, natural rubber, butyl rubbers, butadiene-styrene copolymer rubbers, nitrile rubbers, neoprene rubbers, polybutadiene rubbers, and polyisoprene rubbers.
3. The elastomeric rocket motor insulation of claim 1 , wherein the elastomer comprises EPDM rubber.
4. The elastomeric rocket motor insulation of claim 1 , wherein the at least one curative coagent comprises at least one metal salt of an ethylenically unsaturated carboxylic acid.
5. The elastomeric rocket motor insulation of claim 1 , wherein the at least one curative coagent comprises zinc diacrylate or zinc dimethacrylate.
6. The elastomeric rocket motor insulation of claim 1 , wherein the at least one curative coagent is present in an effective amount to impart upon the elastomeric rocket motor insulation, subsequent to cure, a 100% modulus of at least 400 pounds per square inch and a tear resistance of at least 300 pli.
7. The elastomeric rocket motor insulation of claim 1 , wherein the elastomer comprises from about 35 weight percent to about 80 weight percent of a total weight of the elastomeric rocket motor insulation.
8. The elastomeric rocket motor insulation of claim 1 , wherein the at least one peroxide curative is selected from the group consisting of dicumyl peroxide, 2,5-dimethyl-2,5-bis-(t-butylperoxy)hexane, 2,5-dimethyl-2,5-bis-(benzoylperoxy)hexane, 2,5-dimethyl- 2,5-di(t-butylperoxy)-3-hexane, n-butyl-4,4-bis-(t-butylperoxy)valerate, 4,4′-methylbis-(cyclohexylamine)carbomate, 1,1-bis-(t-butylperoxy)-3,3,5-trimethylcyclohexane, α,α′-bis-(t-butylperoxy)diisopropylbenzene, 2,5-dimethyl-2,5-bis-(t-butylperoxy)hexane, and di-t-butyl peroxide.
9. The elastomeric rocket motor insulation of claim 1 , wherein the at least one hydrophobic surface agent comprises at least one of an organohalosilane, a disilazane, an organosilane, a siloxane, a compound having one or more alkylsiloxyl moieties, or combinations thereof.
10. The elastomeric rocket motor insulation of claim 9 , wherein the organohalosilane is selected from the group consisting of dimethyldichlorosilane, methyltrichlorosilane, dimethyldibromosilane, methyltribromosilane, diethyldichlorosilane, ethyltrichlorosilane, dipropyldichiorosilane, diisopropyldichlorosilane, propyltrichlorosilane, dibutyldichlorosilane, and butyltrichlorosilane.
11. The elastomeric rocket motor insulation of claim 9 , wherein the disilazane is hexamethyl-disilazane.
12. The elastomeric rocket motor insulation of claim 9 , wherein the organosilane is selected from the group consisting of trimethoxy-octyl-silane, hexadecyl silane, and methyacryl-silane.
13. The elastomeric rocket motor insulation of claim 9 , wherein the siloxane is selected from the group consisting of octamethyl-cyclo-tetra-siloxane and polydimethylsiloxane.
14. The elastomeric rocket motor insulation of claim 9 , wherein the compound having one or more alkylsiloxyl moieties has one or more trimethylsiloxyl moieties.
15. An elastomeric rocket motor insulation, comprising:
at least one ethylene-propylene-diene monomer (EPDM) rubber, the EPDM rubber being formed from an EPDM polymer cured with at least one peroxide curative and at least one curative coagent, the at least one curative coagent comprising a polyfunctional metal salt for forming organometallic cross-link bonds in the EPDM rubber; and
a filler comprising at least one member selected from the group consisting of silica particles and silicate particles, the filler being treated with at least one hydrophobic surface agent.
16. The elastomeric rocket motor insulation of claim 15 , wherein the EPDM rubber has an ethylene content ranging from 50 weight percent to 70 weight percent.
17. The elastomeric rocket motor insulation of claim 15 , wherein the at least one curative coagent comprises at least one metal salt of an ethylenically unsaturated carboxylic acid.
18. The elastomeric rocket motor insulation of claim 15 , wherein the at least one curative coagent comprises zinc diacrylate or zinc dimethacrylate.
19. The elastomeric rocket motor insulation of claim 15 , wherein the at least one curative coagent is present in an effective amount to impart upon the elastomeric rocket motor insulation, subsequent to cure, a 100% modulus of at least 400 pounds per square inch and a tear resistance of at least 300 pli.
20. The elastomeric rocket motor insulation of claim 15 , wherein the at least one peroxide curative is selected from the group consisting of dicumyl peroxide, 2,5-dimethyl-2,5-bis-(t-butylperoxy)hexane, 2,5-dimethyl-2,5-bis-(benzoylperoxy)hexane, 2,5-dimethyl-2,5-di(t-butylperoxy)-3-hexane, n-butyl-4,4-bis-(t-butylperoxy)valerate, 4,4′-methylbis-(cyclohexylamine)carbomate, 1,1-bis-(t-butylperoxy)-3,3,5-trimethylcyclohexane, αα′-bis-(t-butylperoxy)diisopropylbenzene, 2,5-dimethyl-2,5-bis-(t-butylperoxy)hexane, and di-t-butyl peroxide.
21. The elastomeric rocket motor insulation of claim 15 , wherein the at least one hydrophobic surface agent comprises at least one of an organohalosilane, a disilazane, an organosilane, a siloxane, a compound having one or more alkylsiloxyl moieties, or combinations thereof.
22. The elastomeric rocket motor insulation of claim 21 , wherein the organohalosilane is selected from the group consisting of dimethyldichlorosilane, methyltrichiorosilane, dimethyldibromosilane, methyltribromosilane, diethyldichlorosilane, ethyltrichlorosilane, dipropyldichlorosilane, diisopropyldichlorosilane, propyltrichlorosilane, dibutyldichiorosilane, and butyltrichlorosilane.
23. The elastomeric rocket motor insulation of claim 21 , wherein the disilazane is hexamethyl-disilazane.
24. The elastomeric rocket motor insulation of claim 21 , wherein the organosilane is selected from the group consisting of trimethoxy-octyl-silane, hexadecyl silane, and methyacryl-silane.
25. The elastomeric rocket motor insulation of claim 21 , wherein the siloxane is selected from the group consisting of octamethyl-cyclo-tetra-siloxane and polydimethylsiloxane.
26. The elastomeric rocket motor insulation of claim 21 , wherein the compound having one or more alkylsiloxyl moieties has one or more trimethylsiloxyl moieties.
27. The elastomeric rocket motor insulation of claim 15 , wherein the at least one EPDM rubber comprises from about 35 weight percent to about 80 weight percent of a total weight of the elastomeric rocket motor insulation.