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dc.contributor.author陳煦zh_TW
dc.contributor.authorHsu Chenen_US
dc.date.accessioned2017-10-06T06:18:01Z-
dc.date.available2017-10-06T06:18:01Z-
dc.date.issued1971-04en_US
dc.identifier.urihttp://hdl.handle.net/11536/137467-
dc.description.abstractThe flight of a ballistic missile is idealized by the assumptions that the speed is acquired impulsively at sea level and that drag is absent. With practical long-range rockets the distance traversed under power is usually 5-10% of the total range, and the length of re-entry path in which drag is significant is even smaller. Consequently the impulsive assumption gives a good first approximation both for the range and for the impact errors of long-range rockets.en_US
dc.language.isoen_USen_US
dc.publisher交大學刊編輯委員會zh_TW
dc.titleA Study on the Range and Accuracy of Long-Rang Ballistic Missilesen_US
dc.typeCampus Publicationsen_US
dc.identifier.journal交大學刊zh_TW
dc.identifier.journalSCIENCE BULLETIN NATIONAL CHIAO-TUNG UNIVERSITYen_US
dc.citation.volume5en_US
dc.citation.issue1en_US
dc.citation.spage121en_US
dc.citation.epage128en_US
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