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MIL-DTL-27723F
PROBE, TOTAL TEMPERATURE, DEICEABLE
Organization:
DLA - GS1 - DLA Aviation - Richmond
Year: 2013
Abstract: This document covers the requirements for total temperature probes capable of operating during atmospheric icing conditions.Intended Use: The total temperature probe covered by this specification is intended for use in aircraft to determine the total temperature developed by adiabatic heating of the air due to the motion of the aircraft, both during and in the absence of atmospheric icing conditions.
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| contributor author | DLA - GS1 - DLA Aviation - Richmond | |
| date accessioned | 2017-09-04T17:23:13Z | |
| date available | 2017-09-04T17:23:13Z | |
| date copyright | 2013.07.16 | |
| date issued | 2013 | |
| identifier other | ZYKNFFAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/146441 | |
| description abstract | This document covers the requirements for total temperature probes capable of operating during atmospheric icing conditions.Intended Use: The total temperature probe covered by this specification is intended for use in aircraft to determine the total temperature developed by adiabatic heating of the air due to the motion of the aircraft, both during and in the absence of atmospheric icing conditions. | |
| language | English | |
| title | MIL-DTL-27723F | num |
| title | PROBE, TOTAL TEMPERATURE, DEICEABLE | en |
| type | standard | |
| page | 16 | |
| status | Not for New Design | |
| tree | DLA - GS1 - DLA Aviation - Richmond:;2013 | |
| contenttype | fulltext |