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
12.5%
Rate breakdown
9903.05.4912.5%Except for products described in headings 9903.05.85–9903.05.92, articles the product of Japan, with an ad valorem (or ad valorem equivalent) rate of duty under column 1 less than 12.5 percent, as provided for in U.S. note 52 to this subchapter
Import Tips
• Classify per specific thrust and power ratings; provide vacuum test data; check ECCN for dual-use export controls