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Characteristics and close-range exploration methods of near- Earth asteroid 2016HO_(3)
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作者 He Zhang Fei Li +3 位作者 Linzhi Meng Fuming Zeng Xiaoyu Jia Yu’ang Liu 《Astronomical Techniques and Instruments》 CSCD 2024年第1期42-51,共10页
The characteristics of asteroids are vital parameters for planning asteroid exploration missions.These characteristics have been explored in close range for some typical asteroids,and are summarized in the article.Thi... The characteristics of asteroids are vital parameters for planning asteroid exploration missions.These characteristics have been explored in close range for some typical asteroids,and are summarized in the article.This allows estimates of the characteristics of asteroid 2016HO_(3),the target of the first Chinese asteroid exploration mission,Tianwen 2.We obtain 80 characteristic parameters in 9 categories and analyze their impacts on the mission.By comparing three close-range exploration modes,we provide advantages and disadvantages of each,and propose suitable methods for the exploration of 2016HO_(3).Owing to the weak gravity and small size of 2016HO_(3),a combination of multiple hovering positions and active orbiting is recommended for scientific exploration. 展开更多
关键词 Near-Earth asteroid 2016ho_(3) Tianwen 2 Close-range exploration CHARACTERISTICS
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Ho_(3)NiSi_(2)合金相关系和相结构及磁性研究
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作者 陈湘 王静 +3 位作者 王晓燏 刘莉 肖洋 谭文兵 《中国有色金属学报》 EI CAS CSCD 北大核心 2022年第5期1383-1390,共8页
本文在分析XRD谱、等温磁化曲线和等磁场变温磁化曲线的基础上,主要研究Ho_(3)NiSi_(2)合金的相结构、磁性相变和磁热性能。结果表明:采用不同方法制备的Ho_(3)NiSi_(2)合金中,第二相Ho_(5)Si_(3)含量存在明显差异,主相的原子占位也存... 本文在分析XRD谱、等温磁化曲线和等磁场变温磁化曲线的基础上,主要研究Ho_(3)NiSi_(2)合金的相结构、磁性相变和磁热性能。结果表明:采用不同方法制备的Ho_(3)NiSi_(2)合金中,第二相Ho_(5)Si_(3)含量存在明显差异,主相的原子占位也存在一定的差异。在低磁场下,Ho_(3)NiSi_(2)合金存在两个磁相变,一个是T_(SR)=12 K的自旋重取向转变,另一个是居里温度为T_(C)=39 K的铁磁−顺磁二级相变。在等温磁化过程中,存在磁场诱导的磁自旋重取向态向正常铁磁态转变的现象,因而在磁熵变(−ΔS_(M))−温度(T)图中,分别在T_(S)和T_(C)附近出现了两个同向的磁熵变峰,且在0~5 T磁场下,T_(SR)和T_(C)温度附近的最大磁熵变可分别达5.3 J/(kg·K)和12.7 J/(kg·K)。由于两种临界温度不同的磁相变会引起合金的制冷温跨增大,进而表现出大的相对制冷能力(RCP);在0~5 T磁场下,Ho_(3)NiSi_(2)合金的制冷温跨和相对制冷能力分别为57.2 K和375.5 J/kg。 展开更多
关键词 ho_(3)NiSi_(2)合金 磁相变 磁热效应
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MgO-Yb_(2)O_(3)-Ho_(2)O_(3)三元烧结助剂对氮化硅陶瓷结构及性能的影响
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作者 王建军 孙峰 +4 位作者 庄英华 廖圣俊 姜常玺 王再义 周立娟 《陶瓷学报》 CAS 北大核心 2022年第3期441-447,共7页
采用气压烧结法,通过调整MgO-Yb_(2)O_(3)-Ho_(2)O_(3)中Yb_(2)O_(3)和Ho_(2)O_(3)的添加比例(0wt.%~6wt.%),研究三元烧结助剂体系下Ho_(2)O_(3)对氮化硅陶瓷XRD物相、显微结构以及导热性能的作用机理。研究结果表明:添加不同比例的Ho_(... 采用气压烧结法,通过调整MgO-Yb_(2)O_(3)-Ho_(2)O_(3)中Yb_(2)O_(3)和Ho_(2)O_(3)的添加比例(0wt.%~6wt.%),研究三元烧结助剂体系下Ho_(2)O_(3)对氮化硅陶瓷XRD物相、显微结构以及导热性能的作用机理。研究结果表明:添加不同比例的Ho_(2)O_(3),陶瓷样品二次相的种类及结晶程度发生显著变化。随着Ho_(2)O_(3)添加量的增加,β-Si_(3)N_(4)晶粒尺寸呈细化趋势,进而使氮化硅陶瓷断裂强度增大,最大为(802±15)MPa;断裂韧性降低,最大为(7.62±0.12)MPa·m^(1/2)。与Yb_(2)O_(3)相比,Ho_(2)O_(3)的加入更易形成玻璃相,从而降低样品结晶度和热导率。 展开更多
关键词 MgO-Yb_(2)O_(3)-ho_(2)O_(3) 三元添加剂 热导率 断裂韧性
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Ho_(2)O_(3)/BiOBr复合光催化剂的制备及光催化性能
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作者 康巧梅 王慧珍 《云南民族大学学报(自然科学版)》 CAS 2021年第3期219-223,共5页
以氧化钬、溴化钠、五水硝酸铋等试剂作为原材料,选用水热法,制备Ho_(2)O_(3)/BiOBr复合光催化剂.通过紫外可见漫反射及红外光谱分析对催化剂进行表征,考察Ho_(2)O_(3)与BiOBr的质量投配比、水热反应时间、制备温度及溶液pH等工艺条件... 以氧化钬、溴化钠、五水硝酸铋等试剂作为原材料,选用水热法,制备Ho_(2)O_(3)/BiOBr复合光催化剂.通过紫外可见漫反射及红外光谱分析对催化剂进行表征,考察Ho_(2)O_(3)与BiOBr的质量投配比、水热反应时间、制备温度及溶液pH等工艺条件对亚甲基蓝溶液降解率的影响.结果表明:Ho_(2)O_(3)/BiOBr复合催化剂的能带隙为2.59 eV;当Ho_(2)O_(3)与BiOBr的质量投配比为10%、水热反应时间为12 h、制备温度为160℃、亚甲基蓝溶液pH=11、投加量为0.05 g,在500 W氙灯照射下时,80 min后亚甲基蓝溶液降解率达95.6%.经4次的重复使用后,Ho_(2)O_(3)/BiOBr复合催化剂对亚甲基蓝溶液的降解率达到81.3%. 展开更多
关键词 水热法 ho_(2)O_(3)/BiOBr复合剂 亚甲基蓝溶液 光催化
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反相微乳液法制备纳米Ho_(2)O_(3)的研究
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作者 董国桢 何金桂 +2 位作者 袁志刚 赵连祥 苏德生 《当代化工研究》 2022年第24期177-179,共3页
稀土氧化物的纳米化是当今纳米科技研究的热点领域之一。本文采用AOT/正丁醇/环己烷/氯化钬(氢氧化铵)反相微乳液体系制备Ho_(2)O_(3)纳米颗粒,并采用FTIR、XRD、SEM等手段对产物的结构、形貌进行表征。结果表明:产物为立方相的Ho_(2)O_... 稀土氧化物的纳米化是当今纳米科技研究的热点领域之一。本文采用AOT/正丁醇/环己烷/氯化钬(氢氧化铵)反相微乳液体系制备Ho_(2)O_(3)纳米颗粒,并采用FTIR、XRD、SEM等手段对产物的结构、形貌进行表征。结果表明:产物为立方相的Ho_(2)O_(3),尺寸为50-100nm之间;当AOT与正丁醇质量比为1:1时,颗粒形状最为规则且分散性最好;加液顺序为先水相后油相时,产物主要为片状;沉淀剂浓度增大,颗粒的粒径越小,形状越规则。 展开更多
关键词 反相微乳液 纳米颗粒 ho2O3 AOT 制备
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Co-orbital transition of 2016 HO_(3) 被引量:1
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作者 Yi Qi Dong Qiao 《Astrodynamics》 EI CSCD 2023年第1期3-14,共12页
In this paper,we investigate the orbital behavior of the transition between the quasisatellite(QS)and horseshoe(HS)motions of 2016 HO3.Based on the phase space structure in the Sun-Earth circular restricted three-body... In this paper,we investigate the orbital behavior of the transition between the quasisatellite(QS)and horseshoe(HS)motions of 2016 HO3.Based on the phase space structure in the Sun-Earth circular restricted three-body problem,we find that the surface of 2016 HO in the torus space is a compound surface formed by QS and HS portions.Its co-orbital motion is therefore a QS-HS transition.2016 HO3 is currently located in a QS state,and its locus clings to the QS portion in the isosurface in agreement with the semi-analytical results.We provide a criterion to separate the QS and HS stages in the transition and obtain accurate incoming and outgoing epochs of the QS motion.We then propose an approximate curve to describe the locus of 2016 HO3 in the w-e projection.Virtual asteroids(VAs)near 2016 HO in the isosurface were created to study the infuence of the initial state of the QS-HS transition.We find that the duration of the QS state is mainly influenced by the loci in the w-e projection.The VAs with large QS durations usually have longer loci across the QS region than those with shorter durations.In addition,although some VAs are close to 2016 HO3 in the w-e projection,their co-orbital behaviors are significantly different from that of the latter.This indicates that the QS-HS transition of 2016 HO3 is sensitive to the(w,e)position. 展开更多
关键词 Asteroid 469219 Kamo'oalewa(2016 ho_(3)) co-orbital motion TRANSITION torus space semi-analytical method
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Trajectory design for a solar-sail mission to asteroid 2016 HO_(3) 被引量:1
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作者 Jeannette Heiligers Juan M.Fernandez +1 位作者 Olive R.Stohlman W.Keats Wilkie 《Astrodynamics》 CSCD 2019年第3期231-246,共16页
This paper proposes the use of solar-sail technology currently under development at NASA Langley Research Center for a CubeSat rendezvous mission with asteroid 2016 HO_(3),a quasi-satellite of Earth.Time-optimal traje... This paper proposes the use of solar-sail technology currently under development at NASA Langley Research Center for a CubeSat rendezvous mission with asteroid 2016 HO_(3),a quasi-satellite of Earth.Time-optimal trajectories are sought for within a 2022–202_(3) launch window,starting from an assumed launcher ejection condition in the Earth-Moon system.The optimal control problem is solved through a particular implementation of a direct pseudo-spectral method for which initial guesses are generated through a relatively simple and straightforward genetic algorithm search on the optimal launch date and sail attitude.The results show that the trajectories take 2.16–4.21 years to complete,depending on the assumed solar-sail reflectance model and solar-sail technology.To assess the performance of solar-sail propulsion for this mission,the trajectory is also designed assuming the use of solar electric propulsion.The resulting fuel-optimal trajectories take longer to complete than the solar-sail trajectories and require a propellant consumption that exceeds the expected propellant capacity onboard the CubeSat.This comparison demonstrates the superior performance of solar-sail technology for this mission. 展开更多
关键词 asteroid 2016 ho_(3) solar sail solar electric propulsion trajectory design trajectory optimization
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CH_(3)O+HO_(2)反应机理和路径的理论研究
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作者 赵慧 路成刚 唐沂珍 《分子科学学报》 CAS 北大核心 2022年第5期415-423,共9页
采用量子化学方法在CCSD(T)/aug-cc-pvtz//ωB97XD/6-311++G(d,p)理论水平下,对CH_(3)O和HO_(2)自由基反应机理和产物进行了研究.计算结果表明,在单重态下,这2个自由基可以直接发生单电子结合反应生成中间体CH_(3)OOOH,随后进一步分解生... 采用量子化学方法在CCSD(T)/aug-cc-pvtz//ωB97XD/6-311++G(d,p)理论水平下,对CH_(3)O和HO_(2)自由基反应机理和产物进行了研究.计算结果表明,在单重态下,这2个自由基可以直接发生单电子结合反应生成中间体CH_(3)OOOH,随后进一步分解生成CH_(2)O_(2)+HO_(2),CH_(3)OH+O_(2),CH_(2)O+HO_(2)O_(2),CHO_(4)+O_(3)和CH_(2)O+HO_(2)+O;同时,还可以发生直接氢抽提反应生成CH_(3)OH+O_(2),其能垒为47.7 kJ·mol^(-1),是单重态反应的主要产物.在三重态下存在2条氢抽提反应,HO_(2)直接抽提CH_(3)O的H原子生成CH_(2)O^(T)+HO_(2)^(T),CH_(3)O抽提HO_(2)的H生成CH_(3)OH^(S)和O^(T),能垒为6.5 kJ·mol^(-1),为三重态反应的主要产物.此外,含时密度泛函理论计算表明在太阳光照射下中间体CH_(3)OH不发生光解.最佳反应路径R8在298 K,1.01×10^(5) Pa条件下的反应速率常数为2.1×10^(-13)cm^(3)·molecule^(-1)·s^(-1). 展开更多
关键词 CH_(3)O ho_(2) 反应机理 量子化学 反应速率常数
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