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SAE AS 8581:2000-03-01

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SAE AS 8581:2000-03-01

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

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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.
Author SAE
Editor SAE
Document type Standard
Format File
ICS 49.050 : Aerospace engines and propulsion systems
Number of pages 19
Set AEROPAKS10U-10
Year 2000
Document history
Country USA
Keyword SAE 8581;SAE AS8581;SAE AS8581;SAE AS 8581