Scientific Mission of the IPEI Payload Onboard ROCSAT-1

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-1 orbit within the latitude band of ¡_35o. The unique features of the 100% duty cycle together wi...

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Veröffentlicht in:TAO : Terrestrial, atmospheric, and oceanic sciences atmospheric, and oceanic sciences, 1999-03, Vol.s (1), p.19-42
Hauptverfasser: 葉惠卿(H. C. Yeh), 蘇信一(S. Y. Su), 葉怡君(Y. C. Yeh), 吳靜美(J. M. Wu), R. A. Heelis, B. J. Holt
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Sprache:eng
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Zusammenfassung: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-1 orbit within the latitude band of ¡_35o. 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.
ISSN:1017-0839
2311-7680
DOI:10.3319/tao.1999.10.s.19(rocsat)