SAE AS 8581:2000-03-01
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SAE AS 8581:2000-03-01

Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust

Summary

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.

Notes

A été annulé par erreur avant 2001-11.

Technical characteristics

Publisher SAE International
Publication Date 03/01/2000
Page Count 19
Themes Aerospace
EAN ---
ISBN ---
Weight (in grams) ---
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