Accession Number : ADA954191
Title : Metallurgical Examination of One-Half Inch Thick Japanese Aircraft Armor Plate from 'Oscar' Aircraft Designation MARK II.
Descriptive Note : Memorandum rept.,
Corporate Author : WATERTOWN ARSENAL LABS MA
Personal Author(s) : Reed,E. L.
Report Date : 01 JUN 1944
Pagination or Media Count : 7
Abstract : The Japanese Aircraft Armor Plate, varying in thickness from .517in to .526in, is composed of a chromium-molydbenum steel of somewhat inferior quality. The plate is homogeneous steel heat treated to a hardness of 495-555 Brinell. The high hardmess level to which the plate was heat treated resulted in the shattering of the plate when subjected to ballistic test. Chromium and molydbenum were not strategic elements at the time of the manufacture of this plate.
Descriptors : AIRCRAFT, ARMOR PLATE, BALLISTICS, CHROMIUM, HEAT, HOMOGENEITY, JAPAN, STEEL, THICKNESS
Subject Categories : Aircraft
Metallurgy and Metallography
Distribution Statement : APPROVED FOR PUBLIC RELEASE