Low volume fraction, enhanced energy release scaffolds for energetic material
US-2024262765-A1 · Aug 8, 2024 · US
US8950329B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8950329-B2 |
| Application number | US-201213726462-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 24, 2012 |
| Priority date | Dec 24, 2012 |
| Publication date | Feb 10, 2015 |
| Grant date | Feb 10, 2015 |
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An electrically operated propellant is configured to ignite and extinguish over a range of pressures. In examples, the electrically operated propellant is included in a gas generation system having a combustion chamber and at least two electrodes coupled with the propellant. The electrically operated propellant is configured to ignite at an ignition condition and extinguish under an extinguishing condition. In the ignition condition an electrical input is applied across the electrodes to ignite the electrically operated propellant. In the extinguishing condition the electrical input is interrupted while the pressure within the combustion chamber is greater than 200 psi, and the ignited electrically operated propellant extinguishes.
Opening claim text (preview).
The claimed invention is: 1. A gas generation system with an electrically operated propellant comprising: a combustion chamber; at least two electrodes configured for coupling with an electrical power source; an electrically operated propellant within the combustion chamber, the electrically operated propellant is configured to extinguish at pressures greater than 200 psi, the at least two electrodes are coupled with the electrically operated propellant; and wherein the elec…
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