本指南旨在提供航空航天用可充电锂电池系统设计和开发时应使用的方法的基本概述。电池系统包括电池芯、监控和控制电子设备以及电池充电器（如适用）。本文介绍的方法适用于作为原始或补充型式认证或军用机身鉴定一部分的已安装设备。

This AIR is intended to provide a basic overview of methodologies that should be utilized when undertaking the design and development of rechargeable lithium battery systems for aerospace applications. The battery system includes the battery cells, monitoring and control electronics, and battery charger as applicable. The methodologies presented herein apply to ¿¿¿installed¿¿¿ equipment which would be part of the original or supplemental type certification or military airframe qualification.