Hybrid Rocket Motor Grain Case from Japan
Filament-wound composite pressure vessel housing solid fuel grain and liquid oxidizer injection system in hybrid rocket motors. Classifies under HTS 8412.90.9050 for hybrid reaction engine parts.
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
• Burst pressure test reports (>1000 psi) and hybrid propellant interface specs confirm classification
• Composite layup diagrams showing oxidizer ports distinguish from solid rocket cases
• Mark as 'propellant tank-engine interface component' in commercial invoice