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8412.90.90.50/Solid Rocket Motor Combustion Chamber/Mexico

Solid Rocket Motor Combustion Chamber from Mexico

High-strength steel combustion chamber for solid propellant rocket motors, containing the burning propellant to produce high-pressure gases. Classified under HTS 8412.90.9050 as a core part of reaction engines other than turbojets used in space and defense applications.

Duty Rate — Mexico → United States

10%

Rate breakdown

9903.05.5510%Section 301 (forced labor) — additional 10% ad valorem on products of Mexico
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Import Tips

• Include propellant compatibility test reports and pressure ratings in import documentation to substantiate reaction engine use

• Check for dual-use restrictions under Wassenaar Arrangement; may require end-user certificates

• Label clearly as 'not for turbojet engines' to prevent reclassification during customs review

Solid Rocket Motor Combustion Chamber from Mexico — Import Duty Rate | HTS 8412.90.90.50