DC Field | Value | Language |
---|---|---|
dc.contributor.author | Rang, Seongmin | ko |
dc.contributor.author | Jeong, Junyeong | ko |
dc.contributor.author | Bhosale, Vikas Khandu | ko |
dc.contributor.author | Kwon, Sejin | ko |
dc.date.accessioned | 2022-09-19T09:00:13Z | - |
dc.date.available | 2022-09-19T09:00:13Z | - |
dc.date.created | 2022-09-19 | - |
dc.date.created | 2022-09-19 | - |
dc.date.created | 2022-09-19 | - |
dc.date.issued | 2022-12 | - |
dc.identifier.citation | FUEL, v.330 | - |
dc.identifier.issn | 0016-2361 | - |
dc.identifier.uri | http://hdl.handle.net/10203/298627 | - |
dc.description.abstract | Hypergolic solid fuels and hydrogen peroxide oxidizers have attracted considerable attention for the development of safe hybrid rocket propulsion systems. In this study, a new approach was explored to develop a safe hypergolic hybrid propulsion system using industrial-grade hydrogen peroxide (similar to 70 wt%). Initially, the pro-pulsion performance of different hypergolic solid fuels with an industrial-grade hydrogen peroxide was calcu-lated using the NASA CEA code to find an appropriate propellant combination. The theoretical specific impulse of the hypergolic solid fuel was 27.8 % over hydrazine and 13.4 % over LMP-103S. Based on theoretical investigations, hypergolic solid fuels, named such as HSF-1 to HSF-10, were fabricated using molding and pressing methods. The ignition delay time was measured using the drop-test method. Interestingly, HSF-3 and HSF-4 exhibited very short ignition delay times of 4.92 and 8.75 ms, respectively, with industrial-grade hydrogen peroxide. In addition, the drop test results of hypergolic solid fuel with varying compression pressure in the pressing method confirmed that a pressure above the compressive strength of the binder shortens the ignition delay times deviation. Further, HSF was also ignited even at low concentration of IGHP (>40 wt%); opens the new area of research in combustion science. Overall, low-toxicity hypergolic solid fuels and industrial-grade hydrogen peroxide are promising alternatives to conventional toxic hypergolic propellants. | - |
dc.language | English | - |
dc.publisher | ELSEVIER SCI LTD | - |
dc.title | Reactivity of hypergolic hybrid solid fuel with industrial grade hydrogen peroxide | - |
dc.type | Article | - |
dc.identifier.wosid | 000849732800001 | - |
dc.identifier.scopusid | 2-s2.0-85135860043 | - |
dc.type.rims | ART | - |
dc.citation.volume | 330 | - |
dc.citation.publicationname | FUEL | - |
dc.identifier.doi | 10.1016/j.fuel.2022.125543 | - |
dc.contributor.localauthor | Kwon, Sejin | - |
dc.contributor.nonIdAuthor | Bhosale, Vikas Khandu | - |
dc.description.isOpenAccess | N | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordAuthor | Hypergolic fuel | - |
dc.subject.keywordAuthor | Low toxicity fuel | - |
dc.subject.keywordAuthor | Industrial grade hydrogen peroxide | - |
dc.subject.keywordAuthor | Hybrid propellant | - |
dc.subject.keywordPlus | IGNITION | - |
dc.subject.keywordPlus | PROPELLANTS | - |
dc.subject.keywordPlus | COMBUSTION | - |
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