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
10%
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
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