The object of the test was to verify the structural adequacy of the forward section of the liquid oxygen tank under simulated ground and flight conditions. (Author)
Forward Body Substantiation Test
1959
19 pages
Report
No indication
English
Manufacturing Processes & Materials Handling , Structural Mechanics , Rocket Propellants , Propellant tanks , Structural properties , Launch vehicles , Models(Simulations) , Liquid rocket oxidizers , Performance(Engineering) , Pressurization , Loads(Forces) , Shear stresses , Moments , Strain(Mechanics) , Deflection , Buckling , Strain gages , Atlas
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