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Calculation of Basic Design Parameters and Structure of a Reactive Penetrator Intended for Movement in Lunar Soil
Russian Aeronautics Pub Date : 2021-03-12 , DOI: 10.3103/s1068799820040182
V. A. Zagovorchev , P. F. Pronina , V. V. Rodchenko

Abstract

A possible design scheme of a lunar reactive penetrator is considered that is able to penetrate into regolith and deliver the scientific equipment to a specified point of the ground volume. The dependences connecting the main design parameters are given. They allow estimating the principal possibility of movement in the ground. Three options for calculating the penetrator model with different types of solid propellant are presented and recommendation for required propellant volume is given.



中文翻译:

打算在月球土壤中运动的反应渗透器的基本设计参数和结构的计算

摘要

考虑到一种可能的月球反应性穿透器设计方案,该方案能够穿透泥土并将科学设备输送到地面体积的指定点。给出了连接主要设计参数的依赖性。它们可以估计在地下运动的主要可能性。提出了三种计算不同类型固体推进剂渗透剂模型的方法,并给出了所需推进剂体积的建议。

更新日期:2021-03-15
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