1999
DOI: 10.1007/s00585-999-1513-3
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EDI electron time-of-flight measurements on Equator-S

Abstract: Abstract. We present the ®rst electron time-of-¯ight measurements obtained with the Electron Drift Instrument (EDI) on Equator-S. These measurements are made possible by amplitude-modulation and coding of the emitted electron beams and correlation with the signal from the returning electrons. The purpose of the time-of-¯ight measurements is twofold. First, they provide the drift velocity, and thus the electric ®eld, when the distance the electrons drift in a gyro period becomes suciently large. Second, they pr… Show more

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Cited by 6 publications
(12 citation statements)
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References 9 publications
(2 reference statements)
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“…Further development led to a time resolution much shorter than the spin period of the spacecraft [ Paschmann et al , 1997]. This improved Electron Drift Instrument (EDI) was first put aboard Equator‐S [ Quinn et al , 1999; Paschmann et al , 1999]. The same type of instrument was flown also on the Cluster spacecraft, which consist of four spacecraft (SC 1, 2, 3, and 4).…”
Section: Introductionmentioning
confidence: 99%
“…Further development led to a time resolution much shorter than the spin period of the spacecraft [ Paschmann et al , 1997]. This improved Electron Drift Instrument (EDI) was first put aboard Equator‐S [ Quinn et al , 1999; Paschmann et al , 1999]. The same type of instrument was flown also on the Cluster spacecraft, which consist of four spacecraft (SC 1, 2, 3, and 4).…”
Section: Introductionmentioning
confidence: 99%
“…The EDI (Paschmann et al, 1997(Paschmann et al, , 2001) onboard Cluster consists of two electron gun/detector units placed on opposite sides of the spacecraft, similar to that flown on the Equator-S spacecraft (Paschmann et al, 1999). Amplitude-modulated electron beams are fired by the two guns in specific directions.…”
Section: R Nakamura Et Al: Fgm-edi Calibration Onboard Clustermentioning
confidence: 99%
“…The drift step, d = v d T g , during the gyration time T g (drift velocity: v d ) is a direct result from EDI measurements: small d can be determined by triangulation, based on the two beamfiring directions (for a detailed description see, Paschmann et al, 1997;Quinn et al, 1999). Large d are more accurately determined by time-of-flight observations of the two beams (Paschmann et al, 1997;Vaith et al, 1998).…”
Section: R Nakamura Et Al: Fgm-edi Calibration Onboard Clustermentioning
confidence: 99%
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“…The triangulation is less accurate for small fields because the drift step becomes large compared to the triangulation base line (e.g. Paschmann et al (1999)). Additionally measurements of the difference of the times of flight for the two beams increase in accuracy; thus the drift velocity can be calculated more precisely.…”
Section: Introductionmentioning
confidence: 99%