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ELECTRICAL POWER SYSTEMS, AIRCRAFT

contributor authorAIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City
date accessioned2017-09-04T18:33:19Z
date available2017-09-04T18:33:19Z
date copyright41205
date issued2012
identifier otherJDRUAFAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=autho1/handle/yse/215509
description abstractThis specification establishes the performance requirements and verifications for electric power subsystems (EPS) for aerospace vehicles, including aircraft, helicopters, and missiles.Intended Use: The requirements in this specification are intended for the development of electrical power systems required by aircraft equipment and subsystems designed to perform combat and support missions in environments unique to military weapons systems. The handbook section (Appendix A) provides rationale, guidance, and lessons learned information that can be used in tailoring requirements to a specific aircraft application.
languageEnglish
titleAFGS-87219Bnum
titleELECTRICAL POWER SYSTEMS, AIRCRAFTen
typestandard
page70
statusActive
treeAIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City:;2012
contenttypefulltext


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