DC Field | Value | Language |
---|---|---|
dc.contributor.author | Bhosale, Vikas K. | ko |
dc.contributor.author | Jeong, Junyeong | ko |
dc.contributor.author | Kwon, Sejin | ko |
dc.date.accessioned | 2019-09-03T03:20:16Z | - |
dc.date.available | 2019-09-03T03:20:16Z | - |
dc.date.created | 2019-09-02 | - |
dc.date.created | 2019-09-02 | - |
dc.date.created | 2019-09-02 | - |
dc.date.issued | 2019-11 | - |
dc.identifier.citation | FUEL, v.255 | - |
dc.identifier.issn | 0016-2361 | - |
dc.identifier.uri | http://hdl.handle.net/10203/266599 | - |
dc.description.abstract | Exploring novel green hypergolic fuels ignited with hydrogen peroxide (H2O2) offers a number of opportunities in space propulsion with regard to replacing conventional toxic propellant combinations. The green hypergolic fuels, B-H bond-rich zwitterions and ionic liquids (ILs) were synthesized; their hypergolic reactivity was investigated with 95% H2O2. Remarkably, ammonia borane (AB) and 1-ethyl-3-methyl imidazolium borohydride ([EMIM][BH4]) exhibited the lowest ignition delay times of 8.1 and 18.5 ms, respectively. For a comprehensive application, the reactivity of liquid and hybrid fuel blends were studied. A liquid fuel blend, [EMIM][BH4] and methyl imidazolium borane (MIMB) (1: 1, w/w) exhibited the ignition delay time of about 35 ms. Further, a solid hybrid fuel blend consisting of 40% AB-paraffin revealed a hypergolic ignition delay time of 9.2 ms. Additionally, the gas phase heat of formation and specific impulse were calculated using G09 and NASA-CEC-71 programs, respectively. The specific impulse of AB was 273 s, which is higher than the stated hypergolic zwitterions. Hence, the B-H bond-rich zwitterions and ILs are promising choices for new generation green hypergolic liquid and hybrid rocket propulsion. | - |
dc.language | English | - |
dc.publisher | ELSEVIER SCI LTD | - |
dc.title | Ignition of boron-based green hypergolic fuels with hydrogen peroxide | - |
dc.type | Article | - |
dc.identifier.wosid | 000479141700074 | - |
dc.identifier.scopusid | 2-s2.0-85068230438 | - |
dc.type.rims | ART | - |
dc.citation.volume | 255 | - |
dc.citation.publicationname | FUEL | - |
dc.identifier.doi | 10.1016/j.fuel.2019.115729 | - |
dc.contributor.localauthor | Kwon, Sejin | - |
dc.contributor.nonIdAuthor | Bhosale, Vikas K. | - |
dc.contributor.nonIdAuthor | Jeong, Junyeong | - |
dc.description.isOpenAccess | N | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordAuthor | Ionic liquid | - |
dc.subject.keywordAuthor | Hypergolic fuel | - |
dc.subject.keywordAuthor | Combustion | - |
dc.subject.keywordAuthor | Hybrid propellant | - |
dc.subject.keywordAuthor | Bipropellant | - |
dc.subject.keywordPlus | IONIC LIQUIDS | - |
dc.subject.keywordPlus | HIGH-PERFORMANCE | - |
dc.subject.keywordPlus | HYDRAZINE | - |
dc.subject.keywordPlus | CYANOBOROHYDRIDE | - |
dc.subject.keywordPlus | ANIONS | - |
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