Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust
NORM herausgegeben am 1.3.2000
Bezeichnung normen: SAE AS8581
Ausgabedatum normen: 1.3.2000
Land: Amerikanische technische Norm
Kategorie: Technische Normen SAE
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.
SUBJECT TAXONOMY: Maintainability and supportability, Engines
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard