Hybrid Rocket Engine for Experimental Vehicles from Japan
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 — Japan → Canada
0%
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