Accession Number : AD0480398
Title : BALLISTIC BEHAVIOR OF ADHESIVELY BONDED HONEYCOMB ALUMINUM PANELS FOR A HIGH PERFORMANCE AIRCRAFT.
Descriptive Note : Final rept. 15 Feb-15 Oct 65,
Corporate Author : TECHNICAL OPERATIONS INC BURLINGTON MA
Personal Author(s) : Rolsten, Robert F.
Report Date : JAN 1966
Pagination or Media Count : 16
Abstract : Adhesively bonded honeycomb panels commonly used with high performance aircraft were subjected to ballistic impact from a military .30 caliber round to analyze target response qualitatively. Structural panels were impacted by a 150-grain projectile traveling at about 300 ft/sec at angles of 15, 45, and 90 degrees. Experimental data on projectile behavior, projectile impact and exit velocities, and damage sustained by the panels were analyzed. The 15-degree impact angle provided the most extensive damage; the projectile, which completely penetrated the panel, produced a high velocity spall fragment, and the honeycomb structure was delaminated. (Author)
Descriptors : *ARMOR PLATE), (*HONEYCOMB CORES, SANDWICH CONSTRUCTION), (*ALUMINUM ALLOYS, (*AIRCRAFT, ARMOR PLATE), ADHESIVES, IMPACT SHOCK, PROJECTILES, TERMINAL BALLISTICS, DAMAGE ASSESSMENT, PANELS, BONDING.
Subject Categories : Ballistics
Distribution Statement : APPROVED FOR PUBLIC RELEASE