本报告旨在鼓励从全球平台的角度设计热管理系统架构。对飞行器、推进系统和航空电子设备的单独采购有助于从热管理角度对飞机进行次优化。为了最大限度地提高飞机的任务性能和预期增长能力，应考虑整体系统效率和有效性。本文件提供了有关飞机热管理系统工程（TMSE）的一般信息。 本文件还讨论了热管理系统工程验证和验证的过程和方法。从热管理的角度来看，飞行器、推进系统和航空电子设备之间的热集成可能特别重要。由于这些因素，本报告旨在鼓励开发更全面的系统工程方法，以帮助消除和/或减少因材料和部件接近温度极限而造成的任务限制。

The intent of this report is to encourage that the thermal management system architecture be designed from a global platform perspective. Separate procurements for air vehicle, propulsion system, and avionics have contributed to the development of aircraft that are sub-optimized from a thermal management viewpoint. In order to maximize the capabilities of the aircraft for mission performance and desired growth capability, overall system efficiency and effectiveness should be considered. This document provides general information about aircraft Thermal Management System Engineering (TMSE). The document also discusses approaches to processes and methodologies for validation and verification of thermal management system engineering.Thermal integration between the air vehicle, propulsion system, and avionics can be particularly important from a thermal management standpoint. Due to these factors, this report is written to encourage the development of a more comprehensive system engineering approach to help eliminate and/or reduce mission limitations as a result of materials and components nearing temperature limits.