File:F-8C with the Digital-Fly-By-Wire Control System - GPN-2002-000194.jpg

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This file has been superseded by 1972-10-07 VoughtF-8 FlyByWire.jpg. It is recommended to use the other file. Please note that deleting superseded images requires consent.
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Description
English: F-8C Digital-Fly-By-Wire Control System was first tested in 1972. The use of electrical and mechanical systems to replace hydraulic systems for aircraft control surface actuation was flight-tested. Today widely used by commercial airliners, theDigital-Fly-By-Wire Control System allows for better maneuver control, smoother rides, and for military aircraft, a higher combat survivability.
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Source Great Images in NASA: Home - info - pic
Author NASA
Other versions Vought F-8 ECN-3276.jpg: 
This image or video was catalogued by Ames Research Center of the United States National Aeronautics and Space Administration (NASA) under Photo ID: Fly-By-Wire.

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This image or video was catalogued by Great Images in NASA of the United States National Aeronautics and Space Administration (NASA) under Photo ID: GPN-2002-000194.

This tag does not indicate the copyright status of the attached work. A normal copyright tag is still required. See Commons:Licensing.
Other languages:

العربية ∙ беларуская (тарашкевіца) ∙ български ∙ Bahaso Jambi ∙ català ∙ čeština ∙ dansk ∙ Deutsch ∙ English ∙ español ∙ فارسی ∙ français ∙ galego ∙ magyar ∙ հայերեն ∙ Bahasa Indonesia ∙ italiano ∙ 日本語 ∙ македонски ∙ മലയാളം ∙ Nederlands ∙ polski ∙ português ∙ русский ∙ sicilianu ∙ slovenščina ∙ Türkçe ∙ українська ∙ 简体中文 ∙ 繁體中文 ∙ +/−

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Public domain This file is in the public domain in the United States because it was solely created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted". (See Template:PD-USGov, NASA copyright policy page or JPL Image Use Policy.)
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current23:28, 9 April 2009Thumbnail for version as of 23:28, 9 April 2009903 × 665 (307 KB)BotMultichillT (talk | contribs){{Information |Description={{en|1=F-8C Digital-Fly-By-Wire Control System was first tested in1972. The use of electrical and mechanical systems to replace hydraulic systems for aircraft control surface actuation was flight-tested. Today widely used by com

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