This specification established the requirements for a 5 second duration, 4500 pound thrust (when determined at 60 °F) solid propellant rocket engine hereinafter specified as 5 S-4500. The 5 S-4500 rocket engine is a moderate duration, low- thrust, self-contained power plant employing a solid propellant. The engine is designed specifically for jet assist take-off (JATO) of aircraft, and to deliver a nominal thrust of 4500 pounds for 5 seconds duration at 60°F and sea level. The engine contains aircraft attachment fittings and an ignition system.
SAE AS 8581-2000由美国机动车工程师协会 US-SAE 发布于 2000-03-01。
SAE AS 8581-2000 在中国标准分类中归属于: V30 发动机总体,在国际标准分类中归属于: 49.050 航空航天发动机和推进系统。
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