Description / Abstract:
This SAE Aerospace Information Report (AIR) provides the
hydraulic and flight-control system designer with the various
design options and techniques that are currently available to
enhance the survivability of military aircraft.
The AIR addresses the following major topics:
a. Design concepts and architecture
b. Design implementation
c. Means to control external leakage
d. Component design
Purpose
This document provides the system design engineer with
information and design considerations to enhance the airborne
hydraulic and control system survivability under combat
conditions.
Field of Application
This AIR will attempt to address the following threats:
a. Typical small arms fire (5.56, 7.62, 12.7, and 14.5 mm
AP)
b. Cannon (20, 30, and 40 mm API/HEI)
Protection against missiles and non-ballistic threats is beyond
the scope of this AIR. This is because except for electronic
counter-measures or evasive maneuvers, no practical technology
exists which allows an aircraft control and hydraulic system to
survive a direct hit by a missile or large caliber anti-aircraft
projectile.