标准摘要
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.Cross Reference: DOD-D-1000,DOD-STD-100,MIL-C-16173,MIL-D-5480,MIL-F-7179,MIL-I-6867,MIL-I-6868,MIL-I-6870,MIL-J-8667,MIL-P-116,MIL-S-28786,MIL-S-5002,MIL-STD-105,MIL-STD-109,MIL-STD-129,MIL-STD-1595,MIL-STD-320,MIL-STD-410,MIL-STD-480,MIL-STD-481,MIL-STD-810,MIL-STD-889
英文名称Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust