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Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust
STANDARD published on 1.3.2000
Designation standards: SAE AS8581
Publication date standards: 1.3.2000
SKU: NS-484699
Country: American technical standard
Category: Technical standards 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
Latest update: 2026-05-17 (Number of items: 2 278 942)
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