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ADS-40A-SP

AIR VEHICLE FLIGHT PERFORMANCE DESCRIPTION

Organization:
ARMY - AV - Aviation and Missile Command
Year: 2000

Abstract: This Standard Practice Aeronautical Design Standard specifies the flight performance data required to document the characteristics and capabilities of an air vehicle. It is the purpose of this standard to provide a clear and complete documentation of the air vehicle flight performance at a level of detail which is consistent with the current stage of design/development of the aircraft. The data requirements are divided into three levels: Level I, Level II, and Level III. LeveL I (the minimum requirement) addresses the level of detail which would be available during the late conceptual design or early preliminary design stage of the air vehicle. Level II addresses the level of detail which would be available during the late preliminary design or early detailed design stage. Level III addresses the level of detail which would be available during the late detailed design or flight test stage. Each level is intended to be consistent with the corresponding level in ADS-10C-SP, Air Vehicle Technical Description Selected sections of this standard may be added to or deleted. This standard is intended to prescribe a minimum quality of documentation at each Level.
This Standard Practice Aeronautical Design Standard is a communications tool. It provides a standard set of the data requirements to provide documentation of air vehicle flight performance. This standard contains a set of requirements designed to be tailored for each contract by the contracting agency. The tailoring process intended for this standard is the deletion of non-applicable requirements.
URI: http://yse.yabesh.ir/std;query=autho162sear3FCDCAC426159DD6E273C9F4A/handle/yse/205543
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    ADS-40A-SP

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contributor authorARMY - AV - Aviation and Missile Command
date accessioned2017-09-04T18:23:08Z
date available2017-09-04T18:23:08Z
date copyright03/13/2000
date issued2000
identifier otherIDGOPAAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=autho162sear3FCDCAC426159DD6E273C9F4A/handle/yse/205543
description abstractThis Standard Practice Aeronautical Design Standard specifies the flight performance data required to document the characteristics and capabilities of an air vehicle. It is the purpose of this standard to provide a clear and complete documentation of the air vehicle flight performance at a level of detail which is consistent with the current stage of design/development of the aircraft. The data requirements are divided into three levels: Level I, Level II, and Level III. LeveL I (the minimum requirement) addresses the level of detail which would be available during the late conceptual design or early preliminary design stage of the air vehicle. Level II addresses the level of detail which would be available during the late preliminary design or early detailed design stage. Level III addresses the level of detail which would be available during the late detailed design or flight test stage. Each level is intended to be consistent with the corresponding level in ADS-10C-SP, Air Vehicle Technical Description Selected sections of this standard may be added to or deleted. This standard is intended to prescribe a minimum quality of documentation at each Level.
This Standard Practice Aeronautical Design Standard is a communications tool. It provides a standard set of the data requirements to provide documentation of air vehicle flight performance. This standard contains a set of requirements designed to be tailored for each contract by the contracting agency. The tailoring process intended for this standard is the deletion of non-applicable requirements.
languageEnglish
titleADS-40A-SPnum
titleAIR VEHICLE FLIGHT PERFORMANCE DESCRIPTIONen
typestandard
page20
statusActive
treeARMY - AV - Aviation and Missile Command:;2000
contenttypefulltext
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DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
yabeshDSpacePersian