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RIT-10 ion thruster

EADS Astrium’s RIT-10 is a 600 W-class radio-frequency gridded-ion thruster flown on ESA’s Artemis spacecraft. ESA’s comparison gives a 30 W/mN power-to-thrust ratio, yielding a normalized nominal thrust of 20 mN; the bounded sources establish Artemis flight heritage and do not assert a current production lifecycle.

Identity

Aliases
RIT 10RIT-10
Domains
spaceflight
Identity Level
model
Kind
electric-thruster
Name
RIT-10 ion thruster
Status
historical

Details

Description
EADS Astrium’s RIT-10 is a 600 W-class radio-frequency gridded-ion thruster flown on ESA’s Artemis spacecraft. ESA’s comparison gives a 30 W/mN power-to-thrust ratio, yielding a normalized nominal thrust of 20 mN; the bounded sources establish Artemis flight heritage and do not assert a current production lifecycle.
Developers
Electric Specs
Input Power Max
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Input Power Min
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Specific Impulse Max
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Specific Impulse Min
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Thrust Max
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Manufacturers
Propellants
xenon

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Creation Time
August 15, 2026 at 02:43:21 UTC
Updated Time
August 21, 2026 at 11:11:03 UTC

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