Rocket Thrust Vector Control Actuator from Canada
Hydraulic or electromechanical actuator system that gimballs rocket nozzles for directional thrust control during flight. This part of reaction engines other than turbojets is covered by HTS 8412.90.9050 for missile and launch vehicle guidance.
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
• Submit detailed specifications showing thrust vectoring function to distinguish from general hydraulic actuators
• Comply with missile technology control regime (MTCR) requirements for actuators exceeding performance thresholds
• Pair with nozzle assembly documentation when importing as a set to maintain consistent classification