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A Simple Model of the Effect of Solar Array Orientation on SMART-1 Floating Potential
DOI: 10.1109/TPS.2006.883405 Bibcode: 2006ITPS...34.2159H

Hilgers, A.; Thiebault, B.; Estublier, D. +6 more

2006 IEEE Transactions on Plasma Science
SMART-1 12
Simulation of the Cluster-Spacecraft Floating Probe Potential
DOI: 10.1109/TPS.2006.883407 Bibcode: 2006ITPS...34.2078T

Escoubet, C. P.; Masson, A.; Laakso, H. +2 more

2006 IEEE Transactions on Plasma Science
Cluster 9
Double-Probe Measurements in Cold Tenuous Space Plasma Flows
DOI: 10.1109/TPS.2006.883375 Bibcode: 2006ITPS...34.2071E

Eriksson, A. I.; Engwall, E.

2006 IEEE Transactions on Plasma Science
Cluster 6
Active Spacecraft Potential Control: Results From the Double Star Project
DOI: 10.1109/TPS.2006.883364 Bibcode: 2006ITPS...34.2046T

Fazakerley, A.; Torkar, K.; Steiger, W.

The ion emitter instrument "active spacecraft potential control" (ASPOC) has been used successfully in several magnetospheric missions including the European Space Agency Cluster Project. An improved version has been developed for the equatorial spacecraft of the Chinese-European Double Star mission (TC-1) launched in December 2003. The modificati…

2006 IEEE Transactions on Plasma Science
DoubleStar 2
Modeling of Plasma Flow Around SMART-1 Spacecraft
DOI: 10.1109/TPS.2006.879098 Bibcode: 2006ITPS...34.2166M

Gengembre, E.; Markelov, G.

SMART-1 is the first European spacecraft that uses electric propulsion as the main propulsion system. The thruster characteristics and plasma measurements performed during SMART-1 mission lay a good foundation for understanding spacecraft/plasma interactions. This paper discusses the applications and modifications of spacecraft plasma interaction …

2006 IEEE Transactions on Plasma Science
SMART-1 1