Axial deceleration-time records have been made in the NOTS Variable-Angle Variable-Pressure Launch¬ing Tank at trajectory angles of 15, 30, 45, 60, and 75 degrees for hemisphere and disk-cylinder noses, at 90 degrees for the hemisphere nose, and at entry velocities of 25, 50, and 75 fps.nMethods for using these data for the predic¬tion of axial acceleration-time function of other missiles are given.nThese records are compared with theory and results of other experiments.
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