摘要
本文介绍了使神号航天飞机乘员逃逸舱目前的方案论证情况和已经进行的有关工作。
This paper describes the present definition of the HERMES crew escape module (C.E.M.) and the relevant tasks already performed. A description of the investigated solution is presented consisting in: the present design, the functioning in normal and emergency cases, extraction from the spaceplane, escape trajectories, landing, ditching recovery and reliability.
