Missile 36D was tested at the Sycamore Canyon Captive Test Site, from 28 October 1959 through 9 February 1960. The purpose of the test program was to study missile tank skin strain characteristics during the thrust build-up transient for both wet and dry engine start configurations. (Author)
Effects of Engine Thrust Transients on XSM-65D Missiles
1960
151 pages
Report
No indication
English
Missile Technology , Structural Mechanics , Surface to surface missiles , Airframes , Propellant tanks , Structural properties , Thickness , Loads(Forces) , Transients , Thrust , Ignition , Liquid rocket propellants , Modulus of elasticity , Strain(Mechanics) , Pressure , Correlation techniques , Atlas , Graphs(Charts) , Skin(Structural) , Xsm-65d missiles
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