Development of an Integrated Environmental Control System

Paper #:
  • 981544

Published:
  • 1998-07-13
Citation:
Letlow, J. and Jenkins, L., "Development of an Integrated Environmental Control System," SAE Technical Paper 981544, 1998, https://doi.org/10.4271/981544.
Pages:
7
Abstract:
An integrated Environmental Control System (ECS) and Thermal Management System (TMS) is under development for the F-22 fighter aircraft. The unique nature of the F-22 ECS/TMS forced a move away from traditional methods of ECS and thermal system development.Unique features of the F-22 ECS/TMS include extensive use of fuel as a heat sink, digital control, and complex and dynamic interactions with other aircraft systems. This paper highlights some of the challenges, achievements, and lessons learned in the F-22 ECS/TMS development process. A brief system description is also provided.
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