AEROspace BATtery design space evaluation and safety verification (AEROBAT)

全电动航天推进系统主要受电池重量、性能和安全性的影响。挑战是保持安全和可靠的水平，同时将增量重量降至最低。针对极其多样化的平台需求优化单个设计是不可能的，需要映射到需求系列的设计概念组合。创新将集中在有效利用多功能和集成设计功能以及坚固的安全案例。该项目将通过示范者的原型，将核心概念成熟到充分验证的模块，阐明哪些概念是可行的和最佳的，并将确定可用于产品的核心设计。

All-electric aerospace propulsion systems are dominated by battery weight, performance and safety. The challenge is maintaining levels of safety and reliability whilst minimising incremental weight. Optimising a single design for extremely diverse platform requirements is not possible and a portfolio of design concepts mapped to requirement families is needed. Innovation will be centred on the effective use of multifunctional and integrated design features with a robust safety case. The project will mature core concepts to fully verified modules clarifying which concepts are viable and optimal, through prototypes for demonstrators and will define core designs that can be exploited into products.