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Variable Specific Impulse Magnetoplasma Rocket (VASIMR) Prototype from Mexico

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 — Mexico → United States

10%

Rate breakdown

9903.05.5510%Section 301 (forced labor) — additional 10% ad valorem on products of Mexico

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 Mexico — Import Duty Rate | HTS 8412.10.00.90