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Descripción
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| The objective of the research program is to design, optimize and develop a space plasma thruster based on helicon-radio-frequency technology and its application to a nano-satellite for attitude and position control. Moreover a detailed feasibility study will be also conducted to evaluate the possibility of using the plasma thruster to heat and decompose hydrazine. The feasibility study will asses the possibility of building up a combined-two-mode-thruster able to operate in the low-thrust high-efficiency plasma-mode and high-thrust low-efficiency hydrazine mode. Only the plasma thruster will be developed and fully tested during this study. | |
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Internacional
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Si |
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Tipo de proyecto
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Proyectos y convenios en convocatorias públicas competitivas |
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Entidad financiadora
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EUROPEAN COMMISSION |
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Nacionalidad Entidad
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Sin nacionalidad |
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Tamaño de la entidad
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Desconocido |
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Fecha concesión
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01/12/2008 |