SAE AIR1083A PDF | Request Standard
Historical

SAE AIR1083A

HYDRAULIC SYSTEM SURVIVABILITY FOR MILITARY AIRCRAFT

Standard by SAE International, 1991-11-01

Available Formats:

Availability: Immediate Download

Language: English

License Type: Single User

Updates: Not Included

SAE AIR1083A

AIR1083A.pdf

About This Item

This report supplies data on various survivability design approaches and techniques to provide a broad frame of reference for future fluid power designers. Before the designer embarks on the overall system design, a comprehensive understanding of the total hostile environment in which the air vehicle is to operate is mandatory. The overall approach is heavily dependent upon the level of threat, small arms versus medium, or heavy caliber antiaircraft projectiles, missile, single or multiple hit survivability and the projected angle of fire. Overall aircraft stability is a factor which dictates recovery speed from any given failure and limits the magnitude of transient disturbances in the control system. The designer should strive to achieve at a minimum a system which allows high performance type aircraft to obtain a quasi-stable period following total control loss to allow safe ejection of the air crew.
SKU: a080513e2736

  • Publication Date: 1991-11-01
  • Standard Status: historical
  • Publisher: SAE International
  • Document Type: Aerospace Standard
  • Subject: Fixed-wing aircraft, Auxiliary power units, Flight control actuators, Fly-by-wire control systems, Heat resistant materials, Control systems, Hydraulic equipment, Electrical systems,
  • Official SAE: Doi link
  • New Version Available: AIR1083C (2024-04-05)
  • Previous Version: AIR1083B (2007-05-23)
  • This Version: AIR1083A (1991-11-01)
  • Previous Version: AIR1083 (1969-10-01)

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