MIL-STD-2102A
AIRCREW ESCAPE PROPULSION SYSTEMS, VIBRATION AND SHOCK TESTS FOR
| contributor author | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD) | |
| date accessioned | 2017-09-04T17:33:36Z | |
| date available | 2017-09-04T17:33:36Z | |
| date copyright | 08/18/1980 | |
| date issued | 1980 | |
| identifier other | DDBQDAAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho162sear3FCDC52731854DD6EFDEC014A/handle/yse/156477 | |
| description abstract | This standard establishes vibration and shock tests of aircrew escape propulsion systems (AEPS) to determine if the systems are constructed to withstand dynamic vibration and shock stresses expected during service use, handling, and transportation. | |
| language | English | |
| title | MIL-STD-2102A | num |
| title | AIRCREW ESCAPE PROPULSION SYSTEMS, VIBRATION AND SHOCK TESTS FOR | en |
| type | standard | |
| page | 14 | |
| status | Active | |
| tree | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD):;1980 | |
| contenttype | fulltext |

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