Rocket Motor Nozzle from Japan
Ablative composite nozzle for solid-fuel rocket motors used in guided missiles, directing exhaust gases for thrust vectoring. Falls under HTS 9306.90.00.80 as a part of missile projectiles.
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
• Include thrust specifications and missile compatibility in commercial invoice
• Avoid bulk packaging that obscures military end-use from customs inspection