The PEGASES gridded ion-ion thruster physics, performance and predictions
POSTER
Abstract
The PEGASES (Plasma propulsion with Electronegative gases) thruster is a gridded ion thruster that accelerates alternately positively and negatively charged ions to provide thrust. Over the last years various prototypes have been tested, adequate diagnostics have been developed and analytical models and simulations are made to better understand and control the physics involved. The plasma density in the region of the ion-ion plasma predicts that the performance of the PEGASES thruster can be comparable to existing thrusters on the market. We have recently provided the first experimental proof-of-concept, accelerating alternately positive and negative ions from an ion-ion plasma within a 10 kHz cycle. Here we present the state of the art in the PEGASES development and discuss the various physics involved and its possible future in space.
Authors
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Ane Aanesland
Laboratoire de Physique des Plasmas, LPP, CNRS-Ecole Polytechnique
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Dmytro Rafalskyi
LPP, CNRS-Ecole Polytechnique
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Jerome Bredin
Laboratoire de Physique des Plasmas, LPP, CNRS-Ecole Polytechnique
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Pascaline Grondein
Laboratoire de Physique des Plasmas, LPP, CNRS-Ecole Polytechnique
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Noureddine Oudini
LPP, CNRS-Ecole Polytechnique
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P. Chabert
Laboratoire de Physique des Plasmas, LPP-CNRS, LPP, CNRS-Ecole Polytechnique, Ecole Polytechnique