Hall Effect Thruster from Japan
An electric Hall effect thruster ionizes xenon propellant using a radial magnetic field and expels ions via electric acceleration for spacecraft station-keeping. It qualifies under HTS 8412.10.00 as a reaction engine producing thrust by reaction mass expulsion, excluding turbojets.
Duty Rate — Japan → United States
10%
Rate breakdown
9903.03.0110%Except for products described in headings 9903.03.02–9903.03.11, articles the product of any country, as provided for in subdivision (aa) of U.S. note 2 to this subchapter
Import Tips
• Classify per specific thrust and power ratings; provide vacuum test data; check ECCN for dual-use export controls