Scramjet Combustor Diverter from Canada
High-temperature alloy combustor inlet diverter managing supersonic airflow in experimental scramjet (supersonic combustion ramjet) engines for hypersonic vehicles. Advanced reaction engine part per HTS 8412.90.9050.
Duty Rate — Canada → United States
10%
Rate breakdown
9903.05.2910%Section 301 (forced labor) — additional 10% ad valorem on products of Canada
Import Tips
• Mach number performance data (Mach 5+) and shockwave management design prove scramjet function
• Government R&D contract references support experimental engine classification
• Thermal protection system integration details distinguish from turbojet inlets