Hybrid Rocket Propulsion System

A hybrid rocket engine combines solid fuel with liquid oxidizer for controlled thrust in missiles and upper-stage rockets. It is included in HTS 8412.10.00.10 as a reaction engine designed exclusively for missile and rocket applications.

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.

8411.82Lower: 12.5% vs 35%

If incorporates gas turbine elements

Engines with auxiliary turbo-pumps may classify under turbojet or turboprop headings.

9301.10.00Lower: 17.5% vs 35%

If for artillery rocket applications

Military rocket systems complete with warheads fall under Chapter 93 munitions.

9031.80.80Same rate: 35%

If when used primarily for thrust testing

Test stand-integrated engines may shift to measuring/testing apparatus in Chapter 90.

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Import Tips & Compliance

β€’ Conduct origin verification to avoid anti-dumping duties on strategic components

β€’ Label with precise configuration (e.g

β€’ fuel grain type) to prevent reclassification

β€’ Partner with customs brokers experienced in DDTC filings for smooth clearance