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JSSG-2006

AIRCRAFT STRUCTURES

Organization:
NAVY - AS - Naval Air Systems Command
Year: 1998

Abstract: This guide establishes the joint structural performance and verification requirements for the airframe. These requirements are derived from operational and maintenance needs and apply to the airframe structure which is required to function, sustain loads, resist damage and minimize adverse operational and readiness impacts during usage for the entire service life. This usage pertains to both land and ship based operations including take-off, catapult, flight, landing, arrestment, ground handling, maintenance, and flight and laboratory tests. This specification also provides for trade studies and analyses to identify and establish certain structural design parameters and criteria which, as a minimum, are necessary to enable the airframe to meet these structural performance requirements, consistent with the program acquisition plan for force level inventory and life cycle cost.
URI: http://yse.yabesh.ir/std;query=autho162sear3FCDCAC426159DD6E273C9FCD/handle/yse/200444
Subject: Aeroacoustic
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  • NAVY - AS - Naval Air Systems Command
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    JSSG-2006

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contributor authorNAVY - AS - Naval Air Systems Command
date accessioned2017-09-04T18:17:40Z
date available2017-09-04T18:17:40Z
date copyright36098
date issued1998
identifier otherHPRIIAAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=autho162sear3FCDCAC426159DD6E273C9FCD/handle/yse/200444
description abstractThis guide establishes the joint structural performance and verification requirements for the airframe. These requirements are derived from operational and maintenance needs and apply to the airframe structure which is required to function, sustain loads, resist damage and minimize adverse operational and readiness impacts during usage for the entire service life. This usage pertains to both land and ship based operations including take-off, catapult, flight, landing, arrestment, ground handling, maintenance, and flight and laboratory tests. This specification also provides for trade studies and analyses to identify and establish certain structural design parameters and criteria which, as a minimum, are necessary to enable the airframe to meet these structural performance requirements, consistent with the program acquisition plan for force level inventory and life cycle cost.
languageEnglish
titleJSSG-2006num
titleAIRCRAFT STRUCTURESen
typestandard
page497
statusActive
treeNAVY - AS - Naval Air Systems Command:;1998
contenttypefulltext
subject keywordsAeroacoustic
subject keywordsAeroelasticity
subject keywordsAeroservoelasticity
subject keywordsAirframe
subject keywordsBuffet
subject keywordsCarrier suitability
subject keywordsCorrosion
subject keywordsCriteria
subject keywordsCritical parts
subject keywordsDamage tolerance
subject keywordsDevelopment test
subject keywordsDurability
subject keywordsFactor of uncertainty
subject keywordsFasteners
subject keywordsFlaws
subject keywordsForeign object damage
subject keywordsLoads
subject keywordsMargin of safety
subject keywordsMaterial
subject keywordsNondestructive testing and inspection
subject keywordsNuclear
subject keywordsResidual strength
subject keywordsScatter factor
subject keywordsService life
subject keywordsSpectrum
subject keywordsStatic test
subject keywordsStrength
subject keywordsStress
subject keywordsSurvivability
subject keywordsThermal
subject keywordsVibration
subject keywordsVibroacoustic
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