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M00021390
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ENGINE; ROCKET, SOLID PROPELLANT 5 SECOND DURATION, 4500 POUNDS THRUST
SAE International
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Availability date: 10/28/2021
Describes 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.
Published | |
Document Type | Standard |
Status | Current |
Publisher | SAE International |
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ISBN | |
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