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HYDRAULIC SYSTEM SURVIVABILITY FOR MILITARY AIRCRAFT
- Aerospace Standard
- AIR1083A
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
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.
Topic
Data Sets - Support Documents
Title | Description | Download |
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Unnamed Dataset 1 |
Issuing Committee
A-6A2 Military Aircraft Committee
The Military Aircraft Panel is responsible for the development of standards and recommended practices related to the integration of fluid power and actuation technologies into military air vehicles. The panel provides a forum for government engineers, prime contractors, suppliers, and fleet support representatives to exchange technical information and discuss regulatory updates, recent technology developments, lessons learned, and issues related to system development and in service operation.
Reference
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