以HTPB與N2O為燃料的高效率反向渦漩混合式火箭推進燃燒系統研製與驗證
| dc.contributor.author | 吳宗信 | zh_TW |
| dc.contributor.author | WU JONG-SHINN | en_US |
| dc.contributor.department | 國立交通大學機械工程學系（所） | zh_TW |
| dc.date.accessioned | 2016-03-28T08:17:49Z | |
| dc.date.available | 2016-03-28T08:17:49Z | |
| dc.date.issued | 2015 | en_US |
| dc.description.sponsorship | 科技部 | zh_TW |
| dc.identifier.govdoc | MOST103-2221-E009-136-MY2 | zh_TW |
| dc.identifier.uri | https://www.grb.gov.tw/search/planDetail?id=11270482&docId=455024 | en_US |
| dc.identifier.uri | https://ir.lib.nycu.edu.tw/handle/11536/130458 | |
| dc.language.iso | zh_TW | en_US |
| dc.title | 以HTPB與N2O為燃料的高效率反向渦漩混合式火箭推進燃燒系統研製與驗證 | zh_TW |
| dc.title | Development and Verification of High-Performance Dual/Quad Vortical Hybrid Rocket Propulsion Systems Using HTPB and Nitrous Oxide | en_US |
| dc.type | Plan | en_US |
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