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

Full metadata record

DC Field	Value	Language
dc.contributor.author	吳宗信	zh_TW
dc.contributor.author	WU JONG-SHINN	en_US
dc.date.accessioned	2016-03-28T08:17:49Z	-
dc.date.available	2016-03-28T08:17:49Z	-
dc.date.issued	2015	en_US
dc.identifier.govdoc	MOST103-2221-E009-136-MY2	zh_TW
dc.identifier.uri	http://hdl.handle.net/11536/130458	-
dc.identifier.uri	https://www.grb.gov.tw/search/planDetail?id=11270482&docId=455024	en_US
dc.description.sponsorship	科技部	zh_TW
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
dc.contributor.department	國立交通大學機械工程學系（所）	zh_TW
Appears in Collections:	Research Plans