A series of tests was conducted to determine the ultimate capability of Minuteman Third Stage Motor cases having a foreward skirt thickness below a previously specified minimum of 0.158 inch. A full scale motor and a forward skirt specimen were used in this analysis.
Qualification Testing of Wing II Through Wing VI Cases with Thin Forward Skirts
1965
128 pages
Report
Keine Angabe
Englisch
Rocket Engines & Motors , Missile Technology , Surface to surface missiles , Third stage engines , Rocket engine cases , Filament wound construction , Structural members , Thickness , Specifications , Performance(Engineering) , Loads(Forces) , Buckling , Compressive properties , Failure(Mechanics) , Aerodynamic loading , Minuteman , Minuteman 1
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