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