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Mars Science Laboratory - Backshell Interface Plate and Parachute Support Structure Subsystem

机译:火星科学实验室 - 后壳界面板和降落伞支撑结构子系统

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Mars Science Laboratory is a scientific mission to deliver a rover with ten science instruments to the surface of Mars. In order to accomplish this, a Cruise Stage and Entry Vehicle, which is comprised of an Aeroshell and Descent Stage, are used. The Backshell Interface Plate (BIP) interfaces to the Backshell, the Cruise Stage and the Descent Stage. Also attached to the BIP is the Parachute Support Structure (PSS) which interfaces to both structure and soft goods of the Parachute Deceleration System. The primary function of the BIP and PSS is to anchor all of these major subsystems together and provide the structural load paths necessary to support the launch, entry, mortar fire, and parachute inflation loads. The key challenges for this hardware lie in the complex configuration, several unique load cases, multiple load paths, and the magnitude of the loads. This paper will describe the design of the Backshell Interface Plate and Parachute Support Structure as well as the key challenges and how they were met.
机译:火星科学实验室是一种科学使命,可以向火星表面提供10个科学仪器的流动站。为了实现这一点,使用由批次和入口车辆组成的巡航阶段和入口车辆。后壳接口板(BIP)接口到后壳,巡航阶段和下降阶段。还附着在BIP上是降落伞支撑结构(PSS),其界面接口降落伞减速系统的结构和软货。 BIP和PSS的主要功能是将所有这些主要子系统锚定在一起,并提供支持发射,入口,砂浆火和降落伞通胀负荷所需的结构负载路径。这种硬件的关键挑战在复杂的配置中,几个独特的负载箱,多重负载路径和负载的大小。本文将描述后壳界面板和降落伞支撑结构的设计以及关键挑战以及如何满足它们。

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