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MIL-PRF-85725A
RACK, INTEGRATED AVIONICS, FORCED AIR COOLED, GENERAL SPECIFICATION FOR
| contributor author | NAVY - AS - Naval Air Systems Command | |
| date accessioned | 2017-09-04T18:06:53Z | |
| date available | 2017-09-04T18:06:53Z | |
| date copyright | 05/20/1998 | |
| date issued | 1998 | |
| identifier other | GNPBEAAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/189846 | |
| description abstract | This specification covers forced-air-cooled, integrated avionics racks, herein after referred to as racks, used for various military avionics systems. The racks are designed to accommodate Standard Electronic Modules (SEMs) using multiple tiers. Intended Use: These racks are required to withstand forward acceleration values of 4g's and sudden temperature changes from −57°C to +95°C (−70°F to +203°F), which exceed the requirements for commercial aircraft. In addition, these racks must mate with modules and primary and secondary backplanes which are unique to military platforms. A sample of an integrated rack configuration is given in figure 8. | |
| language | English | |
| title | MIL-PRF-85725A | num |
| title | RACK, INTEGRATED AVIONICS, FORCED AIR COOLED, GENERAL SPECIFICATION FOR | en |
| type | standard | |
| page | 25 | |
| status | Active | |
| tree | NAVY - AS - Naval Air Systems Command:;1998 | |
| contenttype | fulltext | |
| subject keywords | Aircraft | |
| subject keywords | Backplane | |
| subject keywords | Electromagnetic | |
| subject keywords | Enclosure | |
| subject keywords | Modules |
