resistojet Thruster for Microsatellites
Electric resistance-heated thruster using decomposed hydrazine, HTS 8412.10.00.90. Reaction engine via thermal gas expansion. Compact design for 1U-3U CubeSats.
Import Duty Rates by Country of Origin
| Origin Country | MFN Rate | Ch.99 Surcharges | Total Effective Rate |
|---|---|---|---|
| π¨π³China | Free | +35.0% | 35% |
| π²π½Mexico | Free | +10.0% | 10% |
| π¨π¦Canada | Free | +10.0% | 10% |
| π©πͺGermany | Free | +10.0% | 10% |
| π―π΅Japan | Free | +10.0% | 10% |
Alternative Classifications
This product could be classified differently depending on its characteristics or intended use.
If classified by electric heater function
Heating elements without propulsion go to Chapter 85.
If as process gas heater
Industrial thermal processing equipment classification.
If spacecraft propulsion part
Integral satellite parts classify under aircraft/spacecraft.
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’ Specify heater element material and temperature profiles
β’ Demonstrate Isp improvement over cold gas baseline
β’ Avoid Chapter 85 by emphasizing integrated reaction nozzle
Related Products under HTS 8412.10.00.90
Variable Specific Impulse Magnetoplasma Rocket (VASIMR) Prototype
RF plasma rocket engine prototype for future Mars missions, under HTS 8412.10.00.90 reaction engines. Magnetic nozzle plasma acceleration system. Research/development unit.
Solid Rocket Motor for Model Rockets
A small solid propellant rocket motor designed for hobbyist model rockets, classified under HTS 8412.10.00.90 as a reaction engine other than turbojets. It generates thrust through the expulsion of high-speed exhaust gases from controlled combustion of solid fuel. Falls under this code due to its reaction engine principle excluding turbojet technology.
Hybrid Rocket Engine for Experimental Vehicles
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.
Pulsed Plasma Thruster for Small Satellites
Electric propulsion system using pulsed plasma arcs for CubeSat attitude control, classified HTS 8412.10.00.90 as reaction engine. Generates thrust via plasma expulsion without turbojet components. Used in low-earth orbit microsatellite missions.
Cold Gas Thruster Module for Spacecraft
Pressurized nitrogen expulsion thruster for satellite station-keeping, HTS 8412.10.00.90 other reaction engines. Reaction thrust from high-velocity gas jet without combustion. Excludes semiconductor processing per notes.
Liquid Apogee Engine for Geostationary Satellites
Bipropellant hydrazine/nitrogen tetroxide engine for orbit raising maneuvers, under HTS 8412.10.00.90. Reaction engine via hypergolic combustion exhaust. Qualified for space launch vehicle upper stages.