Development of an Integrated Environmental Control System

981544

07/13/1998

Event
International Conference On Environmental Systems
Authors Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/981544
Pages
7
Citation
Letlow, J., and Jenkins, L., "Development of an Integrated Environmental Control System," SAE Technical Paper 981544, 1998, https://doi.org/10.4271/981544.
Additional Details
Publisher
Published
Jul 13, 1998
Product Code
981544
Content Type
Technical Paper
Language
English