Please use this identifier to cite or link to this item: https://gnanaganga.inflibnet.ac.in:8443/jspui/handle/123456789/2642
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dc.contributor.authorMandal, Saugata-
dc.contributor.authorHashim, Syed Alay-
dc.contributor.authorRoy, Arnab-
dc.contributor.authorKarmakar, Srinibas-
dc.date.accessioned2024-01-08T03:17:49Z-
dc.date.available2024-01-08T03:17:49Z-
dc.date.issued2023-09-
dc.identifier.issn2667-1344-
dc.identifier.urihttps://doi.org/10.1016/j.fpc.2023.06.001-
dc.identifier.urihttp://gnanaganga.inflibnet.ac.in:8080/jspui/handle/123456789/2642-
dc.description.abstractThis short review article explores the advancement, challenges, and prospects of boron-laden solid fuel for ramjet. The energetic aspect of boron combustion is well known, but the complications associated with its efficient combustion persist and must be overcome to harness its potential completely. The strategies like coating, adding additives, and utilizing boron nanoparticles, which may improve its combustion performance, are widely studied. The latest development in advanced rocket propulsion systems, i.e., using a hybrid fuel-based gas generator for ducted rockets or air augmentation of hybrid rockets, seems a feasible idea; as it can provide two-stage combustion, which may significantly promote and improve the combustion performance of boron hence the specific impulse. Since it utilizes hybrid fuel, it retains its advantages of it as well as its drawbacks. To mitigate these drawbacks, various strategies/suggestions are briefly discussed here. A fundamental aspect of boron combustion must be fully understood and addressed for its applications in advanced propulsion systems.en_US
dc.language.isoenen_US
dc.publisherFirePhysChemen_US
dc.subjectBoronen_US
dc.subjectSolid fuelen_US
dc.subjectRamjeten_US
dc.subjectSolid fuel ramjeten_US
dc.subjectSolid fuel ducted rocketen_US
dc.titleA Short Review of Challenges And Prospects of Boron-Laden Solid Fuels for Ramjet Applicationsen_US
dc.typeArticleen_US
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