MIL-DTL-32186A
EXPLOSIVE SEQUENCE CONTROL
| contributor author | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD) | |
| date accessioned | 2017-09-04T17:42:17Z | |
| date available | 2017-09-04T17:42:17Z | |
| date copyright | 01/03/2012 | |
| date issued | 2012 | |
| identifier other | EAGSTEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho162sear3FCDC52731854DD6EFDEC014A/handle/yse/165305 | |
| description abstract | This specification covers the requirements for the explosive sequence control (ESC), DCU- 241/A NAVAIR Drawing 30003-850AS135.Intended Use: The explosive sequence control (ESC), DCU-241/A was designed to select the ejection mode (normal, solo or aft) for the TC-18 aircraft aircrew escape system. Since the ESC was designed strictly for use in military aircraft, there is no commercial application. | |
| language | English | |
| title | MIL-DTL-32186A | num |
| title | EXPLOSIVE SEQUENCE CONTROL | en |
| type | standard | |
| page | 15 | |
| status | Active | |
| tree | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD):;2012 | |
| contenttype | fulltext | |
| subject keywords | Aircrew escape system | |
| subject keywords | TC-18 aircraft |

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