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8412.10.00.90/Hybrid Rocket Engine for Experimental Vehicles/Mexico

Hybrid Rocket Engine for Experimental Vehicles from Mexico

A hybrid rocket engine using solid fuel and liquid oxidizer for university research rockets, under HTS 8412.10.00.90 as other reaction engines. Thrust produced by combustion in a reaction chamber with nozzle expulsion. Excluded from turbojets per statistical notes.

Duty Rate — Mexico → United States

10%

Rate breakdown

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

• Include burn test data and chemical composition to distinguish from pyrotechnic devices

• File for EAR99 classification or BIS license if exceeding amateur rocket performance limits

• Label clearly as 'research propulsion system' to prevent reclassification as fireworks

Hybrid Rocket Engine for Experimental Vehicles from Mexico — Import Duty Rate | HTS 8412.10.00.90