Polythioether sealants
US-2016032058-A1 · Feb 4, 2016 · US
US10591950B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10591950-B2 |
| Application number | US-201715491433-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 19, 2017 |
| Priority date | Apr 19, 2017 |
| Publication date | Mar 17, 2020 |
| Grant date | Mar 17, 2020 |
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The application relates to a Ramjet solid fuel having an ignition temperature of less than 400° C., the fuel comprising a bis-(ethylene oxy) methane polysulfide polymer (BMPP) and hydroxyl-terminated polybutadiene (HTPB), the copolymer having a BMPP/HTPB weight ratio of from 1/3 to 3/1; and the fuel comprising at least 85 weight % copolymer. The BMPP comprises from 5 to 8 weight percent mercaptan. Furthermore, the BMPP is selected from HS(RSS) a CH 2 CH((SSR) c CSH)CH 2 (SSR) b SH a) where R═—(CH 2 ) 2 OCH 2 O(CH 2 ) 2 — and a+b+c<7; and H(SC 2 H 4 OCH 2 OC 2 H4S) n H where n =7. b)
Opening claim text (preview).
What is claimed is: 1. A Ramjet solid fuel having an ignition temperature of less than 400° C., the fuel consisting essentially of a copolymer of bis-(ethylene oxy) methane polysulfide polymer (BMPP) and hydroxyl-terminated polybutadiene (HTPB); isophorone diisocyanate (IDPI); and butyltin; the copolymer having a BMPP/HTPB weight ratio of from 1/3 to 3/1; and the fuel thus consisting essentially of between 83 and 87 weight % copolymer, between 11 and 16 weight % IPDI (Isophorone diisocyanate), and between 0 and 2% butyltin; wherein the BMPP comprises from 5 to 8 weight percent mercaptan; and wherein BMPP is selected from HS(RSS) a CH 2 CH((SSR) c CSH)CH 2 (SSR) b SH a) Where R═—(CH 2 ) 2 OCH 2 O(CH 2 ) 2 — And a+b+c<7; and H(SC 2 H 4 OCH 2 OC 2 H4S) n H b) Where n=7. 2. The Ramjet solid fuel according to claim 1 , wherein the ignition temperature is less than 312° C.
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