【范围】
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This SAE Aerospace Information Report (AIR) contains information on the thermal design
requirements of airborne avionic systems used in military airborne applications. Methods
are explored which are commonly used to provide thermal control of avionic systems. Both
air and liquid cooled systems are discussed.
1.1 Purpose:
This document describes guidelines for the configuration and design of military aircraft
subsystems that provide cooling to airborne avionic systems and recommendations for the
basic cooling concepts, analytical methods and design practices used for the thermal
design of those airborne avionic systems. The efficient design of the interface between
the airframe system and the avionic system is considered.
1.2 Field of Application:
This document is intended to apply to both designers of airborne avionic equipment and of
airborne environmental control systems.strRefField
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