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.
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Alternative Classifications
This product could be classified differently depending on its characteristics or intended use.
If Spacecraft launched by rocket go to Chapter 88 even for propulsion.
If featuring turbopump feed system
Liquid propellant engines with turbines classify as turbojets/turboprops.
If imported as test article for development
Prototype testing machines may classify under Chapter 90.
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
• Require propellant compatibility certification and shelf-life documentation
• Submit thrust chamber acceptance test reports for Customs verification
• Distinguish from aircraft engines by orbital velocity specifications
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