Solid Propellant Rocket Motor

A solid propellant rocket motor is a reaction engine that uses pre-packed solid fuel to generate thrust for missiles and rockets. It falls under HTS 8412.10.00.10 as it is specifically classified as a missile and rocket engine, distinct from turbojets or other reaction engines.

Import Duty Rates by Country of Origin

Origin CountryMFN RateCh.99 SurchargesTotal Effective Rate
πŸ‡¨πŸ‡³ChinaFree+35.0%35%
πŸ‡²πŸ‡½MexicoFree+10.0%10%
πŸ‡¨πŸ‡¦CanadaFree+10.0%10%
πŸ‡©πŸ‡ͺGermanyFree+10.0%10%
πŸ‡―πŸ‡΅JapanFree+10.0%10%

Alternative Classifications

This product could be classified differently depending on its characteristics or intended use.

8411.99.90Higher: 37.4% vs 35%

If classified as a turbojet component rather than pure rocket

Hybrid engines with turbine elements may shift to turbojet headings in Chapter 84.

9306.90.00Lower: 17.5% vs 35%

If supplied as complete munitions device

When integrated into a finished missile, it may classify under Chapter 93 for bombs and munitions.

Not sure which classification is right?

Our AI classifier can analyze your specific product and recommend the correct HTS code with confidence.

Import Tips & Compliance

β€’ Obtain ITAR export licenses and verify end-user certificates due to strict munitions controls

β€’ Include detailed technical specifications and propulsion system diagrams in documentation

β€’ Avoid misclassification as aircraft parts; confirm exclusive use in missiles or rockets