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CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN

contributor authorNAVY - AS - Naval Air Systems Command
date accessioned2017-09-04T16:32:52Z
date available2017-09-04T16:32:52Z
date copyright03/17/1999
date issued1999
identifier otherUSTMIAAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/96327
description abstractThe 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.
languageEnglish
titleMIL-HDBK-2066num
titleCATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGNen
typestandard
page181
statusActive
treeNAVY - AS - Naval Air Systems Command:;1999
contenttypefulltext


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