This document references:
AIR1168/3 - Aerothermodynamic Systems Engineering and Design
Published by SAE International
on
June 20, 2011
This section presents methods and examples of computing the steady-state heating and cooling loads of aircraft compartments. In a steady-state process the flows of heat throughout the system are...
This document references:
AIR1168/8 - Aircraft Fuel Weight Penalty Due to Air Conditioning
Published by SAE International
on
June 23, 2004
The purpose of this section is to provide methods and a set of convenient working charts to estimate penalty values in terms of take-off fuel weight for any given airplane mission. The curves are for...
This document references:
AIR1277 - COOLING OF MODERN AIRBORNE ELECTRONIC EQUIPMENT
Published by SAE International
on
October 1, 1991
This document contains information on the cooling of modern airborne electronics, emphasizing the use of a heat exchange surface which separates coolant and component. It supplements the information...
This document references:
AIR1811 - LIQUID COOLING SYSTEMS
Published by SAE International
on
September 1, 1985
This publication is applicable to liquid cooling systems of the closed loop type and the expendable coolant type in which the primary function is transporting of heat from its source to a heat sink....
This document references:
AIR1812 - ENVIRONMENTAL CONTROL SYSTEMS LIFE CYCLE COST
Published by SAE International
on
October 1, 1985
This report contains background information on life cycle cost elements and key ECS cost factors. Elements of life cycle costs are defined from initial design phases through operational use....
This document references:
ARP217 - TESTING OF PROTOTYPE AIRPLANE AIR CONDITIONING SYSTEMS
Published by SAE International
on
March 15, 1951
These recommendations are written to cover the testing of air conditioning equipment as installed in the prototype aircraft for the purpose of: A Demonstrating safety of the installation. B...