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MIL-E-8581 Engine, Rocket, Solid Propellant, 5 Second Duration, 4500 Pounds Thrust (S/S By Sae-As8581)This specification established the requirements for a 5 second duration, 4500 pound thrust (when determined at 60 deg. F) solid propellant rocket engine hereinafter specified as 5 S-4500.
For Parts Inquires call Parts Hangar, Inc (727) 493-0744
© Copyright 2015 Integrated Publishing, Inc.
A Service Disabled Veteran Owned Small Business