The information contained herein presents loading characteristics, associated parameters, and methods to be used in calculating the catapulting and arresting loads of MIL-A-8863 and MIL-A-8866 for the design of U.S. Navy airplanes operating from shipboard and shorebased launching and recovery gears. A listing of such gears for which data is contained herein is given in Table 1.
Product Details
Published:
09/25/2014
Number of Pages:
1
File Size:
1 file , 34 KB
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