Use of a Langmuir Probe Instrument on Board a Pico-Satellite
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Authors
Ranvier, S.
Anciaux, M.
Cardoen, P.
Gamby, E.
Bonnewijn, S.
De Keyser, J.
Pieroux, D.
Lebreton J.P.
Discipline
Physical sciences
Subject
Communication satellites
Electric potential
Electron temperature
Langmuir probes
Plasma density
Probes
Satellites
Space flight
Spacecraft
Temperature measurement
Cubesat
Electrical ground
Electrical potential
Extraterrestrial measurements
Measurement techniques
Plasma physics
Plasma temperature
Simultaneous measurement
Orbits
Audience
Scientific
Date
2017Metadata
Show full item recordDescription
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.
Citation
Ranvier, S.; Anciaux, M.; Cardoen, P.; Gamby, E.; Bonnewijn, S.; De Keyser, J.; Pieroux, D.; Lebreton J.P. (2017). Use of a Langmuir Probe Instrument on Board a Pico-Satellite. , IEEE Transactions on Plasma Science, Vol. 45, Issue 8, 2007-2012, DOI: 10.1109/TPS.2017.2700211.Identifiers
scopus: 2-s2.0-85021838603
Type
Article
Peer-Review
Yes
Language
eng