Hall Effect Thruster from China
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 — China → United States
37.5%
Rate breakdown
9903.05.3112.5%Except for products described in headings 9903.05.85–9903.05.92, articles the product of China, as provided for in U.S. note 52 to this subchapter
9903.88.0125%Except as provided in headings 9903.88.05, 9903.88.06, 9903.88.07, 9903.88.08, 9903.88.10, 9903.88.11, 9903.88.14, 9903.88.19, 9903.88.50, 9903.88.52, 9903.88.58, 9903.88.60, 9903.88.62, 9903.88.66, 9903.88.67, 9903.88.68, or 9903.88.69, articles the product of China, as provided for in U.S. note 20(a) to this subchapter and as provided for in the subheadings enumerated in U.S. note 20(b) [to this subchapter]
Import Tips
• Classify per specific thrust and power ratings; provide vacuum test data; check ECCN for dual-use export controls