Anti-Tank Guided Missile Engine
A compact solid rocket motor propelling anti-tank guided missiles (ATGMs) to target armored vehicles. Classified in HTS 8412.10.00.10 as a dedicated missile reaction engine.
Import Duty Rates by Country of Origin
Alternative Classifications
This product could be classified differently depending on its characteristics or intended use.
If as complete rocket launcher ammo
Full missile assemblies with warheads classify under Chapter 93.
If for unmanned ground vehicles
Integrated into robotic platforms, shifts to vehicle parts.
Not sure which classification is right?
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Import Tips & Compliance
• File Electronic Export Information accurately for re-export tracking
• Ensure no dual-use interpretations; emphasize military specification
• Budget for demilitarization inspections if refurbished units
Related Products under HTS 8412.10.00.10
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.
Liquid Bipropellant Rocket Engine
This engine uses separate fuel and oxidizer tanks to mix propellants in a combustion chamber, producing high-thrust exhaust for rocket propulsion. Classified under HTS 8412.10.00.10 for its role in missile and rocket systems as a non-turbojet reaction engine.
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.
Cold Gas Thruster Engine
This simple reaction engine expels pressurized gas for attitude control in missiles and small rockets, without combustion. HTS 8412.10.00.10 covers it as a missile and rocket engine due to its reaction propulsion principle.
Upper Stage Kick Motor
A solid-fuel rocket motor used to provide final velocity adjustments in multi-stage missiles and launch vehicles. It qualifies under HTS 8412.10.00.10 for its specific function as a missile and rocket reaction engine.