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Scientific Mission of the IPEI Payload Onboard ROCSAT-1

中華衛星一號電離層電漿電動儀之科學任務

並列摘要


The Ionospheric Plasma and Electrodynamics Instrument (IPEI) onboard ROCSAT-1 is designed to measure the ion composition, density, temperature and drift velocity at the 600 km altitude along the ROCSAT-1orbit within the latitude band of ±35°. The unique features of the 100% duty cycle together with the 1 kHz sampling rate capability of the IPEI payload will enable us to make a significant contribution to the study the dynamic behavior of low-latitude ionospheric phenomena such as the bottom-side sinusoids, the equatorial spread F and the latitude effect of space weather phenomena during the active phase of Solar Cycle 23.

被引用紀錄


葉重賢(2011)。以薁為懸掛基團之單股降冰片烯高分子〔碩士論文,國立臺灣大學〕。華藝線上圖書館。https://doi.org/10.6342/NTU.2011.02596
何美蓉(2006)。利用福衛一號研究頂部電離層之電漿不規則體〔博士論文,國立中央大學〕。華藝線上圖書館。https://www.airitilibrary.com/Article/Detail?DocID=U0031-0207200917341873
陳立悟(2012)。太空氣象科學儀器酬載II〔碩士論文,國立中央大學〕。華藝線上圖書館。https://www.airitilibrary.com/Article/Detail?DocID=U0031-1903201314445116

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