The Thermal State of an Aerodynamic Decelerator for a Small Spacecraft

机译：小型航天器气动减速器的热态

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Space debris is a growing concern that becomes more urgent with the increase in space exploration. This is the reason for equipping spacecraft with disposal systems. One of the methods for space debris removal is deorbiting a small spacecraft by using a decelerator. This paper presents issue analysis related to a selection of design and technology solutions and temperature analysis for inflatable aerodynamic decelerator (IAD) of small spacecraft.

机译：空间碎片越来越受到关注，随着空间探索的增加，这一问题变得更加紧迫。这就是为航天器配备处置系统的原因。清除空间碎片的方法之一是使用减速器使小型航天器绕轨道旋转。本文介绍与小型航天器的充气式气动减速器（IAD）的设计和技术解决方案选择以及温度分析有关的问题分析。

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来源
《International Conference Complex Systems: Control and Modeling Problems》|2019年|339-342|共4页
会议地点 Samara(RU)
作者
Elizaveta Abramova; Sergey Reznik;
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Bauman Moscow State Technical University Moscow Russia;

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原文格式 PDF
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关键词
aerodynamics; aerospace instrumentation; space debris; space vehicles;

机译：空气动力学航空仪表空间碎片；航天器;

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专利

1. Thermal Protection System Response Uncertainty of a Hypersonic Inflatable Aerodynamic Decelerator [J] . Brune Andrew J., Hosder Serhat, Edquist Karl T., Journal of Spacecraft and Rockets . 2017,第1期

机译：高超音速充气气动减速器的热保护系统响应不确定性
2. Aeroelastic Stability of Thermal Protection System for Inflatable Aerodynamic Decelerator [J] . Goldman Benjamin D., Dowell Earl H., Scott Robert C. Journal of Spacecraft and Rockets . 2015,第1期

机译：充气式气动减速器热保护系统的气动弹性稳定性
3. Effect of static shape deformation on aerodynamics and aerothermodynamics of hypersonic inflatable aerodynamic decelerator [J] . Jinghui Guo, Guiping Lin, Xueqin Bu, Acta astronautica . 2017,第JULa期

机译：静态形状变形对高超声速充气气动减速器空气动力学和空气热力学的影响
4. The Thermal State of an Aerodynamic Decelerator for a Small Spacecraft [C] . Elizaveta Abramova, Sergey Reznik International Conference Complex Systems: Control and Modeling Problems . 2019

机译：用于小型航天器的空气动力学减速器的热状态
5. Uncertainty quantification applied to the analysis and design of a Hypersonic Inflatable Aerodynamic Decelerator for spacecraft reentry. [D] . Brune, Andrew J. 2016

机译：不确定性量化适用于用于航天器再入的高超音速充气气动减速器的分析和设计。
6. VO2-based switchable radiator for spacecraft thermal control [O] . Heungsoo Kim, Kwok Cheung, Raymond C. Y. Auyeung, -1

机译：基于VO2的可切换散热器用于航天器热控制
7. Aerodynamic and Aeroelastic Characteristics of a Tension Cone Inflatable Aerodynamic Decelerator [O] . Clark Ian G., Braun Robert D., Ware Joanne S., 2009

机译：张力锥充气气动减速器的气动和气动弹性特性
8. Post-Flight Aerodynamic and Aerothermal Model Validation of a Supersonic Inflatable Aerodynamic Decelerator. [R] . Tang, C., Muppidi, S., Bose, D., 2015

机译：超音速充气气动减速器的飞行后空气动力学和空气模型验证。

The Thermal State of an Aerodynamic Decelerator for a Small Spacecraft

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