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MIL-DTL-32115A
CARTRIDGE, FIRE EXTINGUISHER, AIRCRAFT, CCU-147/A (WB53)
| contributor author | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD) | |
| date accessioned | 2017-09-04T15:12:51Z | |
| date available | 2017-09-04T15:12:51Z | |
| date copyright | 05/31/2007 | |
| date issued | 2007 | |
| identifier other | LYROBCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/11443 | |
| description abstract | This specification covers the requirements for the manufacture and acceptance of the CCU-147/A Aircraft Fire Extinguisher Cartridge, referred to herein as the "cartridge" Intended Use: The CCU 147/A Aircraft Fire Extinguisher Cartridge (DODIC WB53) provides power to initiate the emergency fire extinguisher system in the helicopter fire extinguisher systems. The cartridge creates gas pressure that separates the split sleeve. Pressure from the fire extinguisher container forces the valve open and releases the fire extinguisher agent. The cartridge is designed for military helicopter use and has no equivalent commercial application. | |
| language | English | |
| title | MIL-DTL-32115A | num |
| title | CARTRIDGE, FIRE EXTINGUISHER, AIRCRAFT, CCU-147/A (WB53) | en |
| type | standard | |
| page | 12 | |
| status | Active | |
| tree | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD):;2007 | |
| contenttype | fulltext |
