完整後設資料紀錄
DC 欄位 | 值 | 語言 |
---|---|---|
dc.contributor.author | 陳煦 | zh_TW |
dc.contributor.author | Hsu Chen | en_US |
dc.date.accessioned | 2017-10-06T06:18:01Z | - |
dc.date.available | 2017-10-06T06:18:01Z | - |
dc.date.issued | 1971-04 | en_US |
dc.identifier.uri | http://hdl.handle.net/11536/137467 | - |
dc.description.abstract | The 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.iso | en_US | en_US |
dc.publisher | 交大學刊編輯委員會 | zh_TW |
dc.title | A Study on the Range and Accuracy of Long-Rang Ballistic Missiles | en_US |
dc.type | Campus Publications | en_US |
dc.identifier.journal | 交大學刊 | zh_TW |
dc.identifier.journal | SCIENCE BULLETIN NATIONAL CHIAO-TUNG UNIVERSITY | en_US |
dc.citation.volume | 5 | en_US |
dc.citation.issue | 1 | en_US |
dc.citation.spage | 121 | en_US |
dc.citation.epage | 128 | en_US |
顯示於類別: | 交大學刊 |