
Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust
NORMA vydaná dňa 1.3.2000
Designation standards: SAE AS8581
Publication date standards: 1.3.2000
Country: American technical standard
Kategória: Technické normy 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