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X3 nested-channel Hall thruster

X3 is a 100-kW-class laboratory Hall thruster with three concentric discharge channels sharing a central cathode. Developed through University of Michigan and NASA collaboration, it explores how nested channels can increase power while limiting the footprint of a high-power thruster. In the published 2017 xenon test campaign at NASA Glenn, all seven channel combinations operated stably across a 5–102 kW total-power test matrix. Maximum measured thrust was 5.4 ± 0.1 N at 99 kW and 400 V; specific impulse ranged from 1,800 to 2,650 s with approximately ±60 s uncertainty. The maximum-thrust point and maximum-power point were separate measurements. First fired in 2013, X3 is documented as research hardware rather than a flown propulsion installation.

Identity

Aliases
X3X3 NHTX3 Nested-channel Hall Thruster
Domains
spaceflight
Identity Level
model
Kind
electric-thruster
Name
X3 nested-channel Hall thruster
Status
historical

Details

Description
X3 is a 100-kW-class laboratory Hall thruster with three concentric discharge channels sharing a central cathode. Developed through University of Michigan and NASA collaboration, it explores how nested channels can increase power while limiting the footprint of a high-power thruster. In the published 2017 xenon test campaign at NASA Glenn, all seven channel combinations operated stably across a 5–102 kW total-power test matrix. Maximum measured thrust was 5.4 ± 0.1 N at 99 kW and 400 V; specific impulse ranged from 1,800 to 2,650 s with approximately ±60 s uncertainty. The maximum-thrust point and maximum-power point were separate measurements. First fired in 2013, X3 is documented as research hardware rather than a flown propulsion installation.
Developers
Electric Specs
Input Power Max
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Input Power Min
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Specific Impulse Max
…
Specific Impulse Min
…
Thrust Max
…
First Run Date
2013
Propellants
xenon

Links

Assets & Meta

Creation Time
October 29, 2026 at 15:17:55 UTC
Updated Time
October 29, 2026 at 15:17:55 UTC

Other

Sources
  • Accessed Date
    2026-10-29
    Note
    2017 ground-test matrix: total power 5–102 kW, maximum thrust 5.4 ± 0.1 N at 99 kW/400 V, and 1,800–2,650 ± 60 s specific impulse. Maximum thrust and maximum power are different test points. First firing in 2013. No flight installation is established.
    Publisher
    NASA Technical Reports Server
    Title
    High-Power Performance of a 100-kW Class Nested Hall Thruster
  • Accessed Date
    2026-10-29
    Note
    Identifies X3 as a three-channel, concentrically nested, 100-kW-class Hall thruster used for laboratory technology development.
    Publisher
    NASA Technical Reports Server
    Title
    Thermal Analysis of the X3 Hall Thruster