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ELECTRIC POWER MONITORS, EXTERNAL, AIRCRAFT

contributor authorNAVY - AS - Naval Air Systems Command
date accessioned2017-09-04T15:20:12Z
date available2017-09-04T15:20:12Z
date copyright07/08/1998
date issued1998
identifier otherMVQBEAAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/20084
description abstractThis specification covers electric power monitors which are installed in aircraft to monitor external electric power to prevent power outside the limits of this specification from being applied to equipment in the aircraft. Intended Use: Electric power monitors are designed to be installed in a variety of military aircraft to monitor external power and prevent the application of poor quality external power to the equipment on board the aircraft. There are two power monitors designed for an AC powered aircraft. One provides a DC output to close a DC external power contactor. The other provides a pass through circuit which can close either an AC or DC external power contactor depending on the requirement. Power monitors designed for DC powered aircraft provide a DC output to close a DC external Power contactor. The electric power monitors are exposed for prolonged periods to extreme seagoing environments not encountered by civilian aircraft. There are no comparable monitors used in commercial aviation.
languageEnglish
titleMIL-PRF-24021Knum
titleELECTRIC POWER MONITORS, EXTERNAL, AIRCRAFTen
typestandard
page36
statusActive
treeNAVY - AS - Naval Air Systems Command:;1998
contenttypefulltext
subject keywordsAlternating current
subject keywordsDirect current


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