Arcjet Thruster for Satellite Station-Keeping from Mexico
Electrothermal ammonia arcjet engine for primary propulsion, under HTS 8412.10.00.90 reaction engines. Plasma arc-heated gas expansion through nozzle. High-efficiency low-thrust space propulsion.
Duty Rate — Mexico → 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
• Provide power conditioning unit integration specifications
• Document specific impulse measurements proving electrothermal reaction
• Distinguish from ion engines by constricted arc mechanism