Hybrid Rocket Propulsion System from Mexico
A hybrid rocket engine that combines solid fuel with liquid oxidizer for controlled thrust in missiles and upper-stage rockets. It is included in tariff item 8412.10.00 as a reaction engine designed for missile and rocket propulsion.
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
• Classify the hybrid rocket propulsion system under tariff item 8412.10.00 as a reaction engine
• Provide the CBSA with documentation showing the combustion process
• Ensure compliance with any controlled goods or aerospace regulations