Solid Rocket Motor from China
A solid rocket motor contains pre-mixed solid propellant like ammonium perchlorate composite that burns to produce hot gases expelled through a nozzle for thrust. Classified under HTS 8412.10.00 as it operates by reaction principles distinct from turbojet cycles, commonly used in missile boosters and launch vehicles.
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
9903.88.0125%Except as provided in headings 9903.88.05, 9903.88.06, 9903.88.07, 9903.88.08, 9903.88.10, 9903.88.11, 9903.88.14, 9903.88.19, 9903.88.50, 9903.88.52, 9903.88.58, 9903.88.60, 9903.88.62, 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(a) to this subchapter and as provided for in the subheadings enumerated in U.S. note 20(b) [to this subchapter]
Import Tips
• Include propellant composition analysis and burn rate data; comply with ATF explosive permits for storage/transport; ensure MIL-STD packaging certifications