Liquid Bipropellant Rocket Engine from Canada
This engine uses separate fuel and oxidizer tanks to mix propellants in a combustion chamber, producing high-thrust exhaust for rocket propulsion. Classified under HTS 8412.10.00.10 for its role in missile and rocket systems as a non-turbojet reaction engine.
Duty Rate — Canada → United States
10%
Rate breakdown
9903.05.2910%Section 301 (forced labor) — additional 10% ad valorem on products of Canada
Import Tips
• Provide material safety data sheets for propellants and ensure hazmat shipping compliance
• Register with BIS for dual-use items and prepare for CFIUS review on national security
• Document thrust ratings and burn times to distinguish from experimental or aircraft engines