Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust
NORMA vydaná dňa 1.3.2000
Označenie normy: SAE AS8581
Dátum vydania normy: 1.3.2000
Krajina: Americká technická norma
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