Scramjet Combustor Diverter from China
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 — China → United States
35%
Rate breakdown
9903.03.0110%Except for products described in headings 9903.03.02–9903.03.11, articles the product of any country, as provided for in subdivision (aa) of U.S. note 2 to this subchapter
9903.88.0325%Except as provided in headings 9903.88.13, 9903.88.18, 9903.88.33, 9903.88.34, 9903.88.35, 9903.88.36, 9903.88.37, 9903.88.38, 9903.88.40, 9903.88.41, 9903.88.43, 9903.88.45, 9903.88.46, 9903.88.48, 9903.88.56, 9903.88.64, 9903.88.66, 9903.88.67, 9903.88.68, or 9903.88.69, articles the product of China, as provided for in U.S. note 20(e) to this subchapter and as provided for in the subheadings enumerated in U.S. note 20(f)
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