Liquid Apogee Engine for Geostationary Satellites from Canada
Bipropellant hydrazine/nitrogen tetroxide engine for orbit raising maneuvers, under HTS 8412.10.00.90. Reaction engine via hypergolic combustion exhaust. Qualified for space launch vehicle upper stages.
Duty Rate — Canada → United States
10%
Rate breakdown
9903.05.2910%Except for products described in headings 9903.05.85–9903.05.93, articles the product of Canada, as provided for in U.S. note 52 to this subchapter
Import Tips
• Require propellant compatibility certification and shelf-life documentation
• Submit thrust chamber acceptance test reports for Customs verification
• Distinguish from aircraft engines by orbital velocity specifications