SAE AS 8581-2000
发动机.5秒固体推进剂4500英镑推力火箭

Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust FSC 2845; Should Be Used Instead of MIL-E-8581A(AS), Which Was Cancelled on 26 May 2000

标准号

SAE AS 8581-2000

发布日期

2000年03月01日

实施日期

废止日期

无

中国标准分类号

V30

国际标准分类号

49.050

发布单位

US-SAE

引用标准

MIL-I-6870-1996 MIL-STD-105-1989 DOD-D-1000 DOD-STD-100 MIL-C-16173 MIL-D-5480 MIL-F-7179 MIL-I-6867 MIL-I-6868 MIL-J-8667 MIL-P-116 MIL-S-5002 MIL-S-28786 MIL-STD-109 MIL-STD-129 MIL-STD-320 MIL-STD-410 MIL-STD-480 MIL-STD-481 MIL-STD-810 MIL-STD-889 MIL

适用范围

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 中可能用到的仪器设备