Design and Performance Assessment of Air Cycle Machine based Self Contained cooling system for Pod based EW Systems on Fighter Aircraft Platforms

Abstract Airborne electronic Warfare (EW) pods installed on outboard stations require a self contained cooling system for thermal management of electronics. This paper brings out the challenges encountered in development of an Air Cycle Machine based liquid cooling system used in a pod based EW suite on a fighter aircraft. The cooling system consists of 3 primary modules; ACM Module, Liquid circulation unit and Electronic control unit. The overall system design requirements are translated to individual module and component level performance requirements, control system modes and health monitoring requirements. The various parameters which affect the performance of the individual component and in turn the cooling system such as inlet & outlet scoop performance, ACM performance, Heat exchanger effectiveness, path losses and pump unit are deliberated in the paper and an analytical model developed to analyze and predict the performance of the system at various altitude and mach conditions is discussed. Finally the experimental test results obtained during ground evaluation at a dedicated cooling system test facility and in flight performance parameters obtained from the 2KW Air cycle machine based liquid cooling system are discussed.