درباره ما
MIL-HDBK-2066
CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN
Organization:
NAVY - AS - Naval Air Systems Command
Year: 1999
Abstract: 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.
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| contributor author | NAVY - AS - Naval Air Systems Command | |
| date accessioned | 2017-09-04T16:32:52Z | |
| date available | 2017-09-04T16:32:52Z | |
| date copyright | 03/17/1999 | |
| date issued | 1999 | |
| identifier other | USTMIAAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/96327 | |
| description abstract | 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. | |
| language | English | |
| title | MIL-HDBK-2066 | num |
| title | CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN | en |
| type | standard | |
| page | 181 | |
| status | Active | |
| tree | NAVY - AS - Naval Air Systems Command:;1999 | |
| contenttype | fulltext |