SAE AS8581

Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust

STANDARD published on 1.3.2000

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The information about the standard:

Designation standards: SAE AS8581
Publication date standards: 1.3.2000
Country: American technical standard
Category: Technical standards SAE

Annotation of standard text SAE AS8581 :

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