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
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
• 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