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
9903.05.5510%Except for products described in headings 9903.05.85–9903.05.92 and 9903.05.94, articles the product of Mexico, as provided for in U.S. note 52 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