Hybrid Rocket Engine for Experimental Vehicles from Mexico
A hybrid rocket engine that combines solid fuel with a liquid oxidizer, designed for university research rockets. Thrust is generated through combustion in a reaction chamber and expulsion through a nozzle, qualifying it as a reaction engine other than turbo-jets under tariff item 8412.10.00.
Duty Rate — Mexico → Canada
0%
PGA flags
No agency flag on this HTS number in the CBSA Single Window matching criteria.
CBSA Single Window matching criteria, unknown
Import Tips
• Ensure the engine is classified as a reaction engine other than turbo-jets and provide technical specifications to the CBSA
• Verify if an export permit is required from the country of origin
• Consider the end-use certificate for research purposes