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Reaction Control System Thruster Valve from Japan

High-response solenoid or piezoelectric valve controlling hypergolic propellant flow in spacecraft reaction control thrusters for attitude control. Part of small reaction engines under HTS 8412.90.9050.

Duty Rate — Japan → United States

12.5%

Rate breakdown

9903.05.4912.5%Section 301 (forced labor) — Japan (col1 rate < 12.5 percent): MFN < 12.5% → total duty capped at 12.5%

Import Tips

Specify response time (<10ms) and propellant compatibility (hydrazine, etc.) to confirm RCS application

Space-qualified certifications (NASA/ESA standards) strengthen classification as reaction engine parts

Prevent classification as generic valves by including thrust chamber integration details