Scientific Mission of the IPEI Payload Onboard ROCSAT-1

  • Author(s): H.C.Yeh,S.Y.Su,Y.C.Yeh, J.M.Wu,R.A.Heelis,B.J.Holt
  • DOI:

    10.3319/TAO.1999.10.S.19(ROCSAT)

  • Keywords: ROCSAT-1, Ionospheric Plasma and Electrodynamics Instrument (IPEI)
Abstract

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.

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