Please use this identifier to cite or link to this item: http://nopr.niscpr.res.in/handle/123456789/5032
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dc.contributor.authorSanghavi, R R-
dc.contributor.authorSundaram, S G-
dc.contributor.authorKulkarni, M W-
dc.contributor.authorAsthana, S N-
dc.contributor.authorBohra, B M-
dc.date.accessioned2009-06-30T09:16:22Z-
dc.date.available2009-06-30T09:16:22Z-
dc.date.issued2005-03-
dc.identifier.issn0975-1084 (Online); 0022-4456 (Print)-
dc.identifier.urihttp://hdl.handle.net/123456789/5032-
dc.description175-180en_US
dc.description.abstractLaser light exhibits specific characteristics in the energy transfer to high-energy materials (HEMs) leading to subsequent decomposition process. A set-up was established for laser ignition. Induction time is one of the critical parameters of the HEMs used for various applications. During this study, it was experimentally determined for TPE based RDX-propellants, which are potential candidates for low vulnerability ammunition. Laser beam from a solid state pulsed Nd-YAG operating at 1.06 mm wavelength was used as energy source. An interesting observation was, increase in ignition delay on incorporation of glycidyl azide prepolymer and decrease in ignition delay on addition of ballistic modifier.en_US
dc.language.isoen_USen_US
dc.publisherCSIRen_US
dc.relation.ispartofseriesB 23 K 26/10en_US
dc.sourceJSIR Vol.64(03) [March 2005]en_US
dc.subjectInduction timeen_US
dc.subjectThreshold energyen_US
dc.subjectEnergy fluenceen_US
dc.subjectTPE based RDX propellantsen_US
dc.titleStudies on ignition of TPE based RDX propellants by laser impulseen_US
dc.typeArticleen_US
Appears in Collections:JSIR Vol.64(03) [March 2005]

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