Liquid Apogee Engine for Geostationary Satellites from Mexico
A bipropellant liquid apogee engine using hydrazine and nitrogen tetroxide for orbit-raising maneuvers of geostationary satellites. It operates as a reaction engine through hypergolic combustion and exhaust expulsion, classified 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
• Provide documentation proving the engine is for space launch vehicle upper stages
• Ensure compliance with Canadian export controls and space agency regulations
• Declare the engine's value and technical data accurately to the CBSA