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MIL-W-81752A

WINDSHIELD SYSTEMS, FIXED WING AIRCRAFT GENERAL SPECIFICATION FOR

Organization:
NAVY - AS - Naval Air Systems Command
Year: 1987

Abstract: This specification establishes the general requirements for the design, performance, installation, and acceptance of windshield systems in fixed wing aircraft. Intended Use: The requirements of this specification are intended for use in designing windshield systems for fixed wing aircraft. The windshield system shall provide clear vision for the pilot(s) and provide protection from environmental and other threats. These requirements apply to the transparency materials, framing, support structure, attachments, and seals.
URI: https://yse.yabesh.ir/std/handle/yse/42845
Subject: Anti-static coating
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    MIL-W-81752A

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contributor authorNAVY - AS - Naval Air Systems Command
date accessioned2017-09-04T15:40:39Z
date available2017-09-04T15:40:39Z
date copyright02/27/1987
date issued1987
identifier otherBAGPDAAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/42845
description abstractThis specification establishes the general requirements for the design, performance, installation, and acceptance of windshield systems in fixed wing aircraft. Intended Use: The requirements of this specification are intended for use in designing windshield systems for fixed wing aircraft. The windshield system shall provide clear vision for the pilot(s) and provide protection from environmental and other threats. These requirements apply to the transparency materials, framing, support structure, attachments, and seals.
languageEnglish
titleMIL-W-81752Anum
titleWINDSHIELD SYSTEMS, FIXED WING AIRCRAFT GENERAL SPECIFICATION FORen
typestandard
page22
statusActive
treeNAVY - AS - Naval Air Systems Command:;1987
contenttypefulltext
subject keywordsAnti-static coating
subject keywordsBinocular disparity
subject keywordsFighter/attack type aircraft
subject keywordsFixed wing aircraft
subject keywordsOptics
subject keywordsWindshield systems
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