Calculation of Main Design Parameters of a Reactive Penetrator Intended for Movement in Lunar Soil
- 作者: Zagovorchev V.A.1, Rodchenkov V.V.1
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隶属关系:
- Moscow Aviation Institute
- 期: 卷 62, 编号 4 (2019)
- 页面: 595-603
- 栏目: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/231146
- DOI: https://doi.org/10.3103/S1068799819040093
- ID: 231146
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详细
The possibility of using penetrators to study the Moon’s subsurface is considered and possible launch options are indicated. Dependencies are given that allow calculating the penetrator mass, penetration depth, and arising overloads with sufficient accuracy. The use of a solid propellant engine on a penetrator is demonstrated.
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作者简介
V. Zagovorchev
Moscow Aviation Institute
编辑信件的主要联系方式.
Email: zagovorchevva@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
V. Rodchenkov
Moscow Aviation Institute
Email: zagovorchevva@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
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