Rocket Thrust Vector Control Actuator from Japan
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 — Japan → United States
12.5%
Rate breakdown
9903.05.4912.5%Except for products described in headings 9903.05.85–9903.05.92, articles the product of Japan, with an ad valorem (or ad valorem equivalent) rate of duty under column 1 less than 12.5 percent, as provided for in U.S. note 52 to this subchapter
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