SAE International - AS8581
Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust
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| Organization: | SAE International |
| Publication Date: | 1 March 2000 |
| Status: | active |
description:
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.
Document History
AS8581
March 1, 2000
Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust
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.