Variable Specific Impulse Magnetoplasma Rocket (VASIMR) Prototype from Japan
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 — Japan → 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
• 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