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8412.10.00.90/Variable Specific Impulse Magnetoplasma Rocket (VASIMR) Prototype/Canada

Variable Specific Impulse Magnetoplasma Rocket (VASIMR) Prototype from Canada

RF plasma rocket engine prototype for future Mars missions, under HTS 8412.10.00.90 reaction engines. Magnetic nozzle plasma acceleration system. Research/development unit.

Duty Rate — Canada → United States

10%

Rate breakdown

9903.05.2910%Except for products described in headings 9903.05.85–9903.05.93, articles the product of Canada, as provided for in U.S. note 52 to this subchapter
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Import Tips

• ITAR Category IV(h) technical data package required

• Include RF power coupling efficiency and magnetic field specs

• Distinguish from Hall thrusters by magnetic confinement method

Variable Specific Impulse Magnetoplasma Rocket (VASIMR) Prototype from Canada — Import Duty Rate | HTS 8412.10.00.90