袁先旭,吴波佼,陈琦,谢昱飞

• 1:中国空气动力研究与发展中心计算所

摘要(Abstract)：

火星探测是当前世界航天发展的热点之一。介绍了火星探测计划的三个历史阶段以及火星探测器的构型演变,分析了火星探测器在进入阶段的火星大气以及遇到的相应气动问题,讨论了国内外针对火星环境气动特性预测的研究方法,并围绕我国的火星探测器稳定性研究提出了建议。

关键词(KeyWords)： 火星大气;探测器;气动特性预测;稳定性

Abstract:

Keywords:

基金项目(Foundation):

作者(Author): 袁先旭,吴波佼,陈琦,谢昱飞

DOI: 10.16338/j.issn.1009-1319.2017.04.18

参考文献(References)：

• [1]M Anyoji,H Nagai,K Asai.Development of low density wind tunnel to simulate atmospheric flight on Mars.AIAA2009-1517
• [2]欧阳致远,肖福根.火星及其环境.航天器环境工程.2012,29(6)
• [3]Michael J Wright,Chun Y Tang,Karl T,et al.A review of aerothermal modeling for mars entry missions.AIAA2010-0443
• [4]郑伟,徐厚泽,钟敏,等.国际火星探测计划进展和中国火星卫星重力测量计划研究.大地测量与地球动力学,2011,31(3)
• [5]火星探测计划.http://baike.m.sogou.com/baike/fullLemma.jsp
• [6]朱仁璋,王鸿芳,泉浩芳,等.美国火星表面探测使命述评.航天器工程,2010(3)
• [7]David W Way,Richard W Powell,Allen Chen,et al.Mars science laboratory entry,descent,and landing system performance.IEEE Aerospace Conference,2006
• [8]杜兰.萤火一号火星探测器的轨道设计和STK仿真.测绘科学技术学报,2009
• [9]Abilleira F,Shidner J.Entry,descent,and landing communications for the 2011 Mars science laboratory.Paper IN1-4,23rd International Symposium on Space Flight Dynamics,Pasadena,CA,2012
• [10]Adam Steltzner,Devin Kipp,Allen Chen,et al.Mars science laboratory entry,descent,and landing system.IEEE Aerospace Conference,2006
• [11]Artem A Dyakonov.Influence of the angle of attack on the aerothermodynamics of the Mars science laboratory.36th AIAA Fluid Dynamics Conference and Exhibit,San Francisco,California,2006
• [12]Matthew Mac Lean,Timothy Wadhams,Michael Holden.Investigation of blunt bodies with CO2test gas including catalytic effects.AIAA 2005-4693
• [13]Thomas J.Experimental hypersonic aerodynamic characteristics of the Mars surveyor 2001 precision lander with flap.AIAA Atmosphere Flight Mechanics Conference and Exhibit,AIAA,2002
• [14]Anyoji M.Aerodynamic measurements in the Mars wind tunnel at Tohoku university.AIAA 2011-852
• [15]杨肖峰.火星探测器气动力热和传热特性研究.中国空气动力研究与发展中心硕士学位论文,2013
• [16]C T Johansen.Comparison of MSL RCS jet computations with flow visualization and velocimetry.AIAA
• [17]Peter A Gnoffo K,James Weilmuenster,et al.Effects of sonic line transition on aerothermodynamics of the Mars pathfinder probe.AIAA 95-1825-CP
• [18]Peter A Liever.CFD prediction of the beagle aerodynamic database.AIAA 2002-0683
• [19]Hadas Porat,Umar A Sheikh,Richard G Morgan,et al.Vacuum ultraviolet and ultraviolet emission spectroscopy measurements for titan and Mars atmospheric entry conditions.AIAA 2013-2647
• [20]Mitcheltree R A.Aerodynamics of the Mars microprobe entry vehicles.AIAA 97-3658
• [21]Antonio Viviani.Aerodynamic analysis of a capsule vehicle for a manned exploration mission to Mars.AIAA2009-7386
• [22]程晓丽,李俊红,王强.空间飞行器在火星再入环境下的气动力特性.宇航学报,2010,31(4)
• [23]吕俊明,苗文博,程晓丽,等.火星大气模型参数对火星科学实验室气动力特性的影响.第十六届全国计算流体力学会议,2014
• [24]袁先旭.非定常流动数值模拟及飞行器动态特性分析研究,中国空气动力研究与发展中心博士学位论文,2002
• [25]Mark Schoenenberger.Ballistic range testing of the Mars exploration rover entry capsule.43rd AIAA Aerospace Sciences Meeting and Exhibit,2005
• [26]Jeff Brown.Free flight testing in support of the MARS smart lander aerodynamics database.Atmospheric Flight Mechanics Conference and Exhibit,AIAA,2002