Solid Propellant Rocket Motor from Japan
A solid propellant rocket motor is a reaction engine that uses pre-packed solid fuel to generate thrust for missiles and rockets. It falls under HTS 8412.10.00.10 as it is specifically classified as a missile and rocket engine, distinct from turbojets or other reaction engines.
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
• Obtain ITAR export licenses and verify end-user certificates due to strict munitions controls
• Include detailed technical specifications and propulsion system diagrams in documentation
• Avoid misclassification as aircraft parts; confirm exclusive use in missiles or rockets