2017
DOI: 10.1093/mnras/stx2232
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Measurements of the electrostatic potential of Rosetta at comet 67P

Abstract: We present and compare measurements of the spacecraft potential (V s/c ) of the Rosetta spacecraft throughout its stay in the inner coma of comet 67P/Churyumov-Gerasimenko, by the Langmuir probe (RPC-LAP) and Ion Composition Analyzer (RPC-ICA) instruments. V s/c has mainly been negative, driven by the high temperature (∼5-10 eV) of the coma photoelectrons. The magnitude of the negative V s/c traces heliocentric, cometocentric, seasonal and diurnal variations in cometary outgassing, consistent with production a… Show more

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Cited by 51 publications
(96 citation statements)
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“…Being negative during the period selected, it repels electrons. In the tenuous neutral density environment encountered at 3 au, for an electron temperature of 7 eV and an electron density of 400 cm −3 , the Debye length is about 1 m. The charge sheath extends typically to a radius of three times the Debye length, that is, to about 3 m for the plasma conditions encountered by Rosetta during the period under study (Odelstad et al 2016). The spacecraft potential field decays therefore beyond the location of the sensors.…”
Section: Rpc-lap Electron Densitymentioning
confidence: 94%
“…Being negative during the period selected, it repels electrons. In the tenuous neutral density environment encountered at 3 au, for an electron temperature of 7 eV and an electron density of 400 cm −3 , the Debye length is about 1 m. The charge sheath extends typically to a radius of three times the Debye length, that is, to about 3 m for the plasma conditions encountered by Rosetta during the period under study (Odelstad et al 2016). The spacecraft potential field decays therefore beyond the location of the sensors.…”
Section: Rpc-lap Electron Densitymentioning
confidence: 94%
“…At U B >− α V S/C , the photoelectron current falls off exponentially with increasing U B , with a characteristic e ‐folding typically on the order of 1–2 V. This regime change at U B =− α V S/C is typically identifiable as a sharp knee in the sweeps, hereafter denoted V ph , from which an estimate of the spacecraft potential can be obtained as V S/C =− V ph / α . α has been shown to generally be in the range 0.7–1 by Odelstad et al (). Such spacecraft potential measurements have previously been used by Odelstad et al (, ) to demonstrate the overall pervasiveness of warm (∼5 eV) electrons in the coma of 67P; in this paper we more carefully examine this during the times when the spacecraft is inside the diamagnetic cavity.…”
Section: Instrumentation and Measurementsmentioning
confidence: 98%
“…α has been shown to generally be in the range 0.7–1 by Odelstad et al (). Such spacecraft potential measurements have previously been used by Odelstad et al (, ) to demonstrate the overall pervasiveness of warm (∼5 eV) electrons in the coma of 67P; in this paper we more carefully examine this during the times when the spacecraft is inside the diamagnetic cavity.…”
Section: Instrumentation and Measurementsmentioning
confidence: 98%
“…RPC-LAP data also indicate the presence of a colder electron population with a temperature below 0.1 eV, which is not considered in this study, since the warm population is dominating the electron flux to the spacecraft (Odelstad et al, 2015(Odelstad et al, , 2017(Odelstad et al, , 2018. The electron temperature has to be chosen carefully, since the spacecraft potential is highly dependent on this value.…”
Section: Plasma Model and Simulation Environmentmentioning
confidence: 99%