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PROBE, TOTAL TEMPERATURE, DEICEABLE

contributor authorDLA - GS1 - DLA Aviation - Richmond
date accessioned2017-09-04T17:23:13Z
date available2017-09-04T17:23:13Z
date copyright2013.07.16
date issued2013
identifier otherZYKNFFAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/146441
description abstractThis 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.
languageEnglish
titleMIL-DTL-27723Fnum
titlePROBE, TOTAL TEMPERATURE, DEICEABLEen
typestandard
page16
statusNot for New Design
treeDLA - GS1 - DLA Aviation - Richmond:;2013
contenttypefulltext


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