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SAE AS8581

Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust
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SAE AS8581

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

PUBLISH DATE 2000
PAGES 19
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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.
SDO SAE: SAE International
Document Number AS8581
Publication Date March 1, 2000
Language en - English
Page Count 19
Revision Level
Supercedes
Committee
Publish Date Document Id Type View
March 1, 2000 AS8581 Revision