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Mission and Design Sensitivities for Human Mars Landers Using Hypersonic Inflatable Aerodynamic Decelerators.

机译：使用高超声速充气气动减速器的人类火星登陆器的任务和设计灵敏度。

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This paper explores the impact of human Mars mission architecture decisions on the design and performance of a lander using the HIAD entry system: (a) Earth departure options, (b) Mars arrival options, (c) Entry Descent and Landing options.

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作者
Polsgrove, T.; Thomas, H. D.; Dwyer Cianciolo, A.; Collins, T.; Samareh, J.;
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年度 2017
页码 1-15
总页数 15
原文格式 PDF
正文语种 eng
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关键词
Aerodynamic brakes; Descent; Human factors engineering; Hypersonics; Inflatable structures; Manned mars missions; Solar electric propulsion; Structural design; Aerocapture; Atmospheric entry; Descent trajectories; Launching sites; Payloads; Reusable spacecraft;

机译：空气动力制动器;下降;人因工程;超音速;充气结构;载人火星任务;太阳能电力推进;结构设计; aerocapture;大气入口;下降轨迹;发射场;有效载荷;可重复使用的航天器;

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专利

1. Uncertainty Analysis of Mars Entry Flows over a Hypersonic Inflatable Aerodynamic Decelerator [J] . Brune Andrew J., West Thomas K., Hosder Serhat, Journal of Spacecraft and Rockets . 2015,第3期

机译：高超音速充气气动减速器上火星进入流的不确定性分析
2. Supersonic Inflatable Aerodynamic Decelerators for Use on Future Robotic Missions to Mars [J] . Ian G. Clark, Allison L. Hutchings, Christopher L. Tanner, Journal of Spacecraft and Rockets . 2009,第2期

机译：用于未来火星机器人任务的超音速充气气动减速器
3. Entry descent and landing systems for small planetary missions: Parametric comparison of parachutes and inflatable systems for the proposed Vanguard Mars mission [J] . E. Allouis, A. Ellery, C.S. Welch Acta astronautica . 2006,第8a11期

机译：小型行星飞行任务的入口下降和着陆系统：拟议的Vanguard Mars飞行任务的降落伞和充气系统的参数比较
4. Mission and design sensitivities for human Mars landers using Hypersonic Inflatable Aerodynamic Decelerators [C] . Tara P. Polsgrove, Herbert D. Thomas, Alicia Dwyer Cianciolo, IEEE Aerospace Conference . 2017

机译：使用高超音速充气气动减速器对人类火星着陆器的任务和设计敏感性
5. Aeroelastic analysis and testing of supersonic inflatable aerodynamic decelerators. [D] . Tanner, Christopher Lee. 2012

机译：超音速充气气动减速器的气动弹性分析和测试。
6. Learning to Live on a Mars Day: Fatigue Countermeasures during the Phoenix Mars Lander Mission [O] . Laura K. Barger, Jason P. Sullivan, Andrea S. Vincent, 2012

机译：学习生活在火星日：凤凰号火星着陆器任务期间的疲劳对策
7. Mission and design sensitivities for human Mars landers using Hypersonic Inflatable Aerodynamic Decelerators [O] . Tara P. Polsgrove, Herbert D. Thomas, Alicia Dwyer Cianciolo, 2017

机译：使用超声波充气空气动力学减速器的人类火星着陆机构的使命与设计敏感性
8. Mission and Design Sensitivities for Human Mars Landers Using Hypersonic Inflatable Aerodynamic Decelerators. [R] . Polsgrove, T. P., Thomas, H. D., Dwyer Ciancio, A., 2017

机译：使用高超声速充气气动减速器的人类火星登陆器的任务和设计灵敏度。

Mission and Design Sensitivities for Human Mars Landers Using Hypersonic Inflatable Aerodynamic Decelerators.

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