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%Section 301 (forced labor) — Japan (col1 rate < 12.5 percent): MFN < 12.5% → total duty capped at 12.5%
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