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SAE AS 8581 : 2000

Current

Current

The latest, up-to-date edition.

ENGINE; ROCKET, SOLID PROPELLANT 5 SECOND DURATION, 4500 POUNDS THRUST

Published date

03-01-2000

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.

DevelopmentNote
Supersedes MIL-E-8581
DocumentType
Standard
PublisherName
SAE International
Status
Current
Supersedes

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