Hybrid Rocket Propulsion System from United States
A hybrid rocket propulsion system that combines solid fuel with liquid oxidizer for controlled thrust in missiles and upper-stage rockets. This reaction engine falls under tariff item 8412.10.00 as a reaction engine other than turbo-jets.
Duty Rate — United States → Canada
0%
Import Tips
• Classify the system under 8412.10.00 as a reaction engine, and be prepared to provide details on the hybrid propellant system to the CBSA
• Verify any permits required for the transport of solid and liquid propellants