Use of a Langmuir Probe Instrument on Board a Pico-Satellite
dc.contributor.author | Ranvier, S. | |
dc.contributor.author | Anciaux, M. | |
dc.contributor.author | Cardoen, P. | |
dc.contributor.author | Gamby, E. | |
dc.contributor.author | Bonnewijn, S. | |
dc.contributor.author | De Keyser, J. | |
dc.contributor.author | Pieroux, D. | |
dc.contributor.author | Lebreton J.P. | |
dc.date | 2017 | |
dc.date.accessioned | 2017-08-04T11:03:08Z | |
dc.date.available | 2017-08-04T11:03:08Z | |
dc.identifier.uri | https://orfeo.belnet.be/handle/internal/5948 | |
dc.description | The sweeping Langmuir probe instrument is a part of the payload of PICo-satellite for atmospheric and space science observations (PICASSO), an ESA in-orbit demonstrator. It includes four thin cylindrical probes whose electrical potential is swept to measure both plasma density and electron temperature together with the spacecraft (S/C) potential. PICASSO is a triple unit CubeSat of dimensions $340.5 mm x 100 mm x 100$ mm. The orbit is expected to be a high inclination low-earth orbit. The main issue implied by the use of a pico-satellite platform for a Langmuir probe instrument is the limited conducting area of the S/C, which leads to S/C charging and drift of the instrument's electrical ground during the measurement. A specific measurement technique that includes the simultaneous measurement of the potential and current of different probes has been developed to retrieve consistent current-voltage characteristics that can be used to estimate the plasma parameters mentioned above. | |
dc.language | eng | |
dc.title | Use of a Langmuir Probe Instrument on Board a Pico-Satellite | |
dc.type | Article | |
dc.subject.frascati | Physical sciences | |
dc.audience | Scientific | |
dc.subject.free | Communication satellites | |
dc.subject.free | Electric potential | |
dc.subject.free | Electron temperature | |
dc.subject.free | Langmuir probes | |
dc.subject.free | Plasma density | |
dc.subject.free | Probes | |
dc.subject.free | Satellites | |
dc.subject.free | Space flight | |
dc.subject.free | Spacecraft | |
dc.subject.free | Temperature measurement | |
dc.subject.free | Cubesat | |
dc.subject.free | Electrical ground | |
dc.subject.free | Electrical potential | |
dc.subject.free | Extraterrestrial measurements | |
dc.subject.free | Measurement techniques | |
dc.subject.free | Plasma physics | |
dc.subject.free | Plasma temperature | |
dc.subject.free | Simultaneous measurement | |
dc.subject.free | Orbits | |
dc.source.title | IEEE Transactions on Plasma Science | |
dc.source.volume | 45 | |
dc.source.issue | 8 | |
dc.source.page | 2007-2012 | |
Orfeo.peerreviewed | Yes | |
dc.identifier.doi | 10.1109/TPS.2017.2700211 | |
dc.identifier.scopus | 2-s2.0-85021838603 |