Hybrid Rocket Engine from Japan
A hybrid rocket engine employs solid fuel with liquid oxidizer, burning to produce gaseous reaction products expelled for thrust in sounding rockets. Falls under HTS 8412.10.00 as chemical reaction engine other than turbojets.
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
• Provide fuel/oxidizer compatibility data; hazardous material shipping papers mandatory; combustion chamber pressure test reports required