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Hybrid Rocket Motor Grain Case from China

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 — China → United States

37.5%

Rate breakdown

9903.88.0325%Except as provided in headings 9903.88.13, 9903.88.18, 9903.88.33, 9903.88.34, 9903.88.35, 9903.88.36, 9903.88.37, 9903.88.38, 9903.88.40, 9903.88.41, 9903.88.43, 9903.88.45, 9903.88.46, 9903.88.48, 9903.88.56, 9903.88.64, 9903.88.66, 9903.88.67, 9903.88.68, or 9903.88.69, articles the product of China, as provided for in U.S. note 20(e) to this subchapter and as provided for in the subheadings enumerated in U.S. note 20(f)
9903.05.3112.5%Section 301 (forced labor) — additional 12.5% ad valorem on products of China

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