SAE AS8581 PDF
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Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust
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.
History
| AS8581 | 2000-03-01 | Latest | Issued |
| ISSUING COMMITTEE | Aerospace Council |
|---|---|
| DATE | 2000-03-01 |
| DOI | |
| ISCURRENT | Current |
| PAGE | 19 |
| PUBLISHER | SAE International |
| REVISED | ISSUED |
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