Rocket Thrust Vector Control Actuator from China
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 — China → United States
35%
Rate breakdown
9903.03.0110%Except for products described in headings 9903.03.02–9903.03.11, articles the product of any country, as provided for in subdivision (aa) of U.S. note 2 to this subchapter
9903.88.0325%Except as provided in headings 9903.88.13, 9903.88.18, 9903.88.33, 9903.88.34, 9903.88.35, 9903.88.36, 9903.88.37, 9903.88.38, 9903.88.40, 9903.88.41, 9903.88.43, 9903.88.45, 9903.88.46, 9903.88.48, 9903.88.56, 9903.88.64, 9903.88.66, 9903.88.67, 9903.88.68, or 9903.88.69, articles the product of China, as provided for in U.S. note 20(e) to this subchapter and as provided for in the subheadings enumerated in U.S. note 20(f)
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