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. 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.
SAE AIR1277B-2005 Referenced Document
SAE AIR1168/10-1992 Thermophysical Characteristics of Working Fluids and Heat Transfer Fluids
SAE AIR1706 The Advanced Environmental Control System (AECS) Computer Program for Steady State Analysis and Preliminary System Sizing*， 2011-02-10 Update
SAE ARP217 TESTING OF PROTOTYPE AIRPLANE AIR CONDITIONING SYSTEMS
STANAG 2895-1990 Extreme Climatic Conditions and Derived Conditions for Use in Defining Design/Test Criteria for NATO Forces Materiel (ED 1; Amendment 1: 07/11/2002; To obtain please contact your national Defense Standardization Office or the NATO Standardization Office w