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.
Subject: Aeroacoustic
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contributor author | NAVY - AS - Naval Air Systems Command | |
date accessioned | 2017-09-04T18:17:40Z | |
date available | 2017-09-04T18:17:40Z | |
date copyright | 36098 | |
date issued | 1998 | |
identifier other | HPRIIAAAAAAAAAAA.pdf | |
identifier uri | http://yse.yabesh.ir/std;query=autho162sear3FCDCAC426159DD6E273C9FCD/handle/yse/200444 | |
description 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. | |
language | English | |
title | JSSG-2006 | num |
title | AIRCRAFT STRUCTURES | en |
type | standard | |
page | 497 | |
status | Active | |
tree | NAVY - AS - Naval Air Systems Command:;1998 | |
contenttype | fulltext | |
subject keywords | Aeroacoustic | |
subject keywords | Aeroelasticity | |
subject keywords | Aeroservoelasticity | |
subject keywords | Airframe | |
subject keywords | Buffet | |
subject keywords | Carrier suitability | |
subject keywords | Corrosion | |
subject keywords | Criteria | |
subject keywords | Critical parts | |
subject keywords | Damage tolerance | |
subject keywords | Development test | |
subject keywords | Durability | |
subject keywords | Factor of uncertainty | |
subject keywords | Fasteners | |
subject keywords | Flaws | |
subject keywords | Foreign object damage | |
subject keywords | Loads | |
subject keywords | Margin of safety | |
subject keywords | Material | |
subject keywords | Nondestructive testing and inspection | |
subject keywords | Nuclear | |
subject keywords | Residual strength | |
subject keywords | Scatter factor | |
subject keywords | Service life | |
subject keywords | Spectrum | |
subject keywords | Static test | |
subject keywords | Strength | |
subject keywords | Stress | |
subject keywords | Survivability | |
subject keywords | Thermal | |
subject keywords | Vibration | |
subject keywords | Vibroacoustic |