航天飞机应急逃生车辆和机构

Shun-Wen Cheng
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引用次数: 0

摘要

本文研究了航天飞机紧急逃生载具的设计。提议的EEV具有反向阿波罗式锥形结构,包含一个载人陀螺仪稳定悬挂旋转球体,并且具有一个可折叠模块。因此,它为宇航员提供了很高的允许重力载荷和生存能力。所提议的EEV具有高容积效率并且是可拆卸的,因此航天飞机仍然可以携带一个大的有效载荷。EEV系统的设计确实大大延长了剩余航天飞机的寿命。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Emergency escape vehicles and mechanisms for space shuttles
This study considers emergency escape vehicles (EEV) design for Space Shuttles. The proposed EEV has the reverse Apollo-style cone configuration, contains a manned gyro-stabilized suspension rotator sphere, and has a collapsible module. Therefore, it gives astronauts a high permissible gravitational loading and survivability. The proposed EEV has high volumetric efficiency and is removable, so the Space Shuttle still can carry a large payload. The designs of the EEV system greatly extend the lifespan of the remaining space shuttle fleet indeed.
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