Solid combustible propellant composition
US-2017267601-A1 · Sep 21, 2017 · US
US12264115B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12264115-B2 |
| Application number | US-201916530042-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 2, 2019 |
| Priority date | Aug 2, 2019 |
| Publication date | Apr 1, 2025 |
| Grant date | Apr 1, 2025 |
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An igniter composition has (i) a source of copper selected from basic copper nitrate, copper oxide, copper hydroxide, and/or copper complex of guanylurea nitrate, (ii) one or more oxidizers, (iii) a binder selected from guanidine nitrate and/or guanylurea nitrate, and (iv) an inorganic fuel comprising an elemental metal or metal hydride selected from the group consisting of: titanium, silicon, aluminum, magnesium, iron, and combinations thereof. The igniter composition may be substantially free of boron or contain minimal amounts of boron. A minimum flame temperature at combustion (T c ) of ≥about 2300K (2,027° C.). Such a mixture may be spray dried to form a powder that is compacted to form a solid igniter composition, such as a pellet or grain. The mixture that is spray dried may have a heat of explosion (HEX) of ≤about 1,000 calories per gram (cal/g). Inorganic fuel can then be added to the spray-dried powder.
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What is claimed is: 1. An igniter composition comprising: (v) a source of copper including at least one of copper hydroxide and a copper complex of guanylurea nitrate; (vi) a plurality of oxidizers that include at least potassium perchlorate (KClO 4 ) and potassium nitrate (KNO 3 ); (vii) a binder selected from the group consisting of: guanidine nitrate, guanylurea nitrate, and combinations thereof; and (viii) an inorganic fuel comprising at least titanium hydride, wherein…
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