AFGS-87219B
ELECTRICAL POWER SYSTEMS, AIRCRAFT
Year: 2012
Abstract: This 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.
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contributor author | AIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City | |
date accessioned | 2017-09-04T18:33:19Z | |
date available | 2017-09-04T18:33:19Z | |
date copyright | 41205 | |
date issued | 2012 | |
identifier other | JDRUAFAAAAAAAAAA.pdf | |
identifier uri | http://yse.yabesh.ir/std;query=autho1/handle/yse/215509 | |
description abstract | This 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. | |
language | English | |
title | AFGS-87219B | num |
title | ELECTRICAL POWER SYSTEMS, AIRCRAFT | en |
type | standard | |
page | 70 | |
status | Active | |
tree | AIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City:;2012 | |
contenttype | fulltext |