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HYDRAULIC FLUID, FIRE RESISTANT; LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE

contributor authorAIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City
date accessioned2017-09-04T18:41:15Z
date available2017-09-04T18:41:15Z
date copyright04/22/2004
date issued2004
identifier otherJWTCFBAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=autho1826AF679D4049A96159DD6E273C9FCD/handle/yse/222827
description abstractThis specification describes the characteristics and provides the requirements for a synthetic hydrocarbon base hydraulic fluid for use in the −54°C to +200°C temperature range in aircraft and missile hydraulic systems. This hydraulic fluid is identified by NATO Code No. H-538 (see 6.5). Intended Use: The hydraulic fluid covered by this specification is intended for use from −54°C to +200°C in automatic pilots, shock absorbers, brakes, flap-control mechanisms, missile hydraulic servo-controlled systems, and other hydraulic systems using synthetic sealing material.
languageEnglish
titleMIL-PRF-87257Bnum
titleHYDRAULIC FLUID, FIRE RESISTANT; LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILEen
typestandard
page17
statusActive
treeAIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City:;2004
contenttypefulltext
subject keywordsadditive
subject keywordshydraulic systems
subject keywordsanti-wear
subject keywordscontamination
subject keywordscorrosion resistant
subject keywordsfire resistant
subject keywordsflash point
subject keywordshydraulic system
subject keywordslubricant
subject keywordsoxidation stability
subject keywordspour point
subject keywordsshear stability
subject keywordsviscosity


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