Hybrid Rocket Engine for Experimental Vehicles from Germany
A hybrid rocket engine using solid fuel and liquid oxidizer for university research rockets, under HTS 8412.10.00.90 as other reaction engines. Thrust produced by combustion in a reaction chamber with nozzle expulsion. Excluded from turbojets per statistical notes.
Duty Rate — Germany → United States
10%
Rate breakdown
9903.05.3910%Section 301 (forced labor) — European Union member state (col1 rate < 10 percent): MFN < 10% → total duty capped at 10%
Import Tips
• Include burn test data and chemical composition to distinguish from pyrotechnic devices
• File for EAR99 classification or BIS license if exceeding amateur rocket performance limits
• Label clearly as 'research propulsion system' to prevent reclassification as fireworks