Pub. L. 106-36, tit. II, subtit. A, ch. 2, sec. 2172

CERTAIN ROCKET ENGINES.

EnactedYear: 1999Length: 65 wordsOfficial source
SEC. 2172. CERTAIN ROCKET ENGINES. Subchapter II of chapter 99 is amended by inserting in numerical sequence the following new heading: 113 STAT. 151 “ 9902.84.12 Dual thrust chamber rocket engines each having a maximum static sea level thrust exceeding 3,550 kN and nozzle exit diameter exceeding 127 cm (provided for in subheading 8412.10.00) .................................... Free No change No change On or before 12/31/2001 ”.
Pub. L. 106-36, tit. II, subtit. A, ch. 2, sec. 2172: CERTAIN ROCKET ENGINES. | Justis AI