Variable Specific Impulse Magnetoplasma Rocket (VASIMR) Prototype
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.
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Alternative Classifications
This product could be classified differently depending on its characteristics or intended use.
If imported as RF transmitter assembly
Radio transmission apparatus supersedes propulsion.
If classified by electromagnet function
Magnetic equipment without reaction thrust.
If laboratory plasma generation equipment
Research physics apparatus classification.
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Import Tips & Compliance
• 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
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