Solid Rocket Motor from Japan
A solid rocket motor contains pre-mixed solid propellant like ammonium perchlorate composite that burns to produce hot gases expelled through a nozzle for thrust. Classified under HTS 8412.10.00 as it operates by reaction principles distinct from turbojet cycles, commonly used in missile boosters and launch vehicles.
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
• Include propellant composition analysis and burn rate data; comply with ATF explosive permits for storage/transport; ensure MIL-STD packaging certifications