Arcjet Thruster for Satellite Station-Keeping from Japan
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 — 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
• Provide power conditioning unit integration specifications
• Document specific impulse measurements proving electrothermal reaction
• Distinguish from ion engines by constricted arc mechanism