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Polar Mesospheric Summer Echo Characteristics in Magnetic Local Time and Height Profiles 磁地方时和高度剖面的极地中间层夏季回波特征
Q3 Earth and Planetary Sciences Pub Date : 2023-09-01 DOI: 10.5140/jass.2023.40.3.101
Young-Sook Lee, Ram Singh, Geonhwa Jee, Young-Sil Kwak, Yong Ha Kim
We conducted a statistical study of polar mesospheric summer echoes (PMSEs) in relation to magnetic local time (MLT), considering the geomagnetic conditions using the K-index (or K). Additionally, we performed a case study to examine the velocity profile, specifically for high velocities (≥ ~100 m/s) varying with high temporal resolution at high K-index values. This study utilized the PMSE data obtained from the mesosphere–stratosphere–troposphere radar located in Esrange, Sweden (63.7°N, 21°E). The change in K-index in terms of MLT was high (K ≥ 4) from 23 to 04 MLT, estimated for the time PMSE was present. During the near-midnight period (0–4 MLT), both PMSE occurrence and signal-to-noise ratio (SNR) displayed an asymmetric structure with upper curves for K ≥ 3 and lower curves for K < 3. Furthermore, the occurrence of high velocities peaked at 3–4 MLT for K ≥ 3. From case studies focusing on the 0–3 MLT period, we observed persistent eastward-biased high velocities (≥ 200 m/s) prevailing for ~18 min. These high velocities were accompanied with the systematic motion of profiles at 85–88 km, including large shear formation. Importantly, the rapid variations observed in velocity could not be attributed to neutral wind effects. The present findings suggest a strong substorm influence on PMSE, especially in the midnight and early dawn sectors. The large zonal drift observed in PMSE were potentially energized by local electromagnetic fields or the global convection field induced by the electron precipitation during substorms.
我们利用K指数(或K)对地磁条件下极地中间层夏季回波(pmse)与磁地方时(MLT)的关系进行了统计研究。此外,我们还进行了一个案例研究,以检查速度剖面,特别是在高K指数值下随高时间分辨率变化的高速(≥100 m/s)。本研究利用位于瑞典Esrange(63.7°N, 21°E)的中流层-平流层-对流层雷达获得的PMSE数据。从PMSE出现的时间来看,从23 MLT到04 MLT, K指数的变化很大(K≥4)。近子夜时段(0 ~ 4 MLT) PMSE发生和信噪比(SNR)均呈现K≥3时上曲线、K <时下曲线的不对称结构;3.此外,当K≥3时,高速的发生在3 - 4 MLT处达到峰值。从0-3 MLT时期的案例研究中,我们观察到持续向东偏的高速(≥200米/秒)持续了约18分钟。这些高速伴随着85-88公里剖面的系统运动,包括大型切变形成。重要的是,观测到的速度的快速变化不能归因于中性风的影响。目前的研究结果表明,亚暴对PMSE有很强的影响,特别是在午夜和黎明时段。在PMSE观测到的大纬向漂移是由局地电磁场或亚暴期间电子沉降引起的全球对流场潜在激发的。
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引用次数: 0
Post Trajectory Insertion Performance Analysis of Korea Pathfinder Lunar Orbiter Using SpaceX Falcon 9 使用SpaceX猎鹰9号的韩国探路者月球轨道器后轨道插入性能分析
Q3 Earth and Planetary Sciences Pub Date : 2023-09-01 DOI: 10.5140/jass.2023.40.3.123
Young-Joo Song, Jonghee Bae, SeungBum Hong, Jun Bang, Donghun Lee
This paper presents an analysis of the trans-lunar trajectory insertion performance of the Korea Pathfinder Lunar Orbiter (KPLO), the first lunar exploration spacecraft of the Republic of Korea. The successful launch conducted on August 4, 2022 (UTC), utilized the SpaceX Falcon 9 rocket from Cape Canaveral Space Force Station. The trans-lunar trajectory insertion performance plays a crucial role in ensuring the overall mission success by directly influencing the spacecraft’s onboard fuel consumption. Following separation from the launch vehicle (LV), a comprehensive analysis of the trajectory insertion performance was performed by the KPLO flight dynamics (FD) team. Both orbit parameter message (OPM) and orbit determination (OD) solutions were employed using deep space network (DSN) tracking measurements. As a result, the KPLO was accurately inserted into the ballistic lunar transfer (BLT) trajectory, satisfying all separation requirements at the target interface point (TIP), including launch injection energy per unit mass (C3), right ascension of the injection orbit apoapsis vector (RAV), and declination of the injection orbit apoapsis vector (DAV). The precise BLT trajectory insertion facilitated the smoother operation of the KPLO’s remainder mission phase and enabled the utilization of reserved fuel, consequently significantly enhancing the possibilities of an extended mission.
本文分析了韩国第一艘月球探测航天器——韩国探路者月球轨道器(KPLO)的跨月轨道插入性能。2022年8月4日(UTC时间),SpaceX公司的猎鹰9号火箭从卡纳维拉尔角空间站成功发射。跨月轨道插入性能直接影响到航天器的星载燃料消耗,对确保整个任务的成功起着至关重要的作用。在与运载火箭(LV)分离后,KPLO飞行动力学(FD)团队对轨道插入性能进行了全面分析。轨道参数信息(OPM)和轨道确定(OD)两种方案均采用深空网络(DSN)跟踪测量。结果表明,KPLO准确地插入弹道月球转移(BLT)轨道,满足目标界面点(TIP)的所有分离要求,包括单位质量发射注入能量(C3)、注入轨道离地点矢量(RAV)赤经、注入轨道离地点矢量(DAV)赤纬。精确的BLT轨道插入促进了KPLO剩余任务阶段的平稳运行,并使储备燃料得以利用,从而大大提高了延长任务的可能性。
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引用次数: 0
Uncertainty Quantification of Thermophysical Property Measurement in Space and on Earth: A Study of Liquid Platinum Using Electrostatic Levitation 空间和地球热物性测量的不确定度量化:利用静电悬浮对液态铂的研究
Q3 Earth and Planetary Sciences Pub Date : 2023-09-01 DOI: 10.5140/jass.2023.40.3.93
Jannatun Nawer, Takehiko Ishikawa, Hirohisa Oda, Chihiro Koyama, Douglas M. Matson
A study of uncertainty analysis was conducted on four key thermophysical properties of molten Platinum using a non-contacting levitation technique. More specifically, this work demonstrates a detailed reporting of the uncertainties associated with the density, volumetric thermal expansion coefficient, surface tension and viscosity measurements at higher temperatures for a widely used refractory metal, Platinum using electrostatic levitation (ESL). The microgravity experiments were conducted using JAXA’s Electrostatic Levitation Furnace (ELF) facility on the International Space Station and the terrestrial experiments were conducted using NASA’s Marshal Space Flight Center’s ESL facility. The performance of these two facilities were then quantified based on the measurement precision and accuracy using the metrological International Standards Organization’s Guide to the Expression of Uncertainty Measurement (GUM) principles.
采用非接触式悬浮技术对熔融铂的四项关键热物性进行了不确定度分析研究。更具体地说,这项工作详细报告了一种广泛使用的难熔金属铂在高温下的密度、体积热膨胀系数、表面张力和粘度测量的不确定性。微重力实验使用JAXA在国际空间站上的静电悬浮炉(ELF)设备进行,地面实验使用美国宇航局马歇尔航天飞行中心的ESL设备进行。然后使用计量国际标准组织的不确定度测量表达指南(GUM)原则,根据测量精度和准确度对这两种设备的性能进行量化。
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引用次数: 0
Response to the Comment by Chandra S on “Interaction of Ion Cyclotron Electromagnetic Wave with Energetic Particles in the Existence of Alternating Electric (AC) Field Using Ring Distribution” 对Chandra S关于“在交变电场存在下离子回旋加速器电磁波与高能粒子相互作用的环形分布”评论的回应
IF 0.5 Q3 Earth and Planetary Sciences Pub Date : 2023-06-01 DOI: 10.5140/jass.2023.40.2.91
K. N. Shukla, J. Kumari, R. S. Pandey
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引用次数: 0
Titius-Bode’s Relation in Exoplanetary Systems 系外行星系统中的提丢斯-波德关系
IF 0.5 Q3 Earth and Planetary Sciences Pub Date : 2023-06-01 DOI: 10.5140/jass.2023.40.2.67
Heon-Young Chang
The Titius-Bode’s relation has been historically successful in predicting the location of Ceres in the solar system, while its physical basis remains hidden. In this study, we attempt to answer the question of whether the Titius-Bode’s relation is universally valid for exoplanetary systems with plural exoplanets. For this purpose, we statistically study the distribution of the ratio of the orbiting periods of two planets in 32 exoplanetary systems hosted by a single star. We only consider the period ratios derived from exoplanets orbiting a single star since celestial objects under investigation are kept as simple as possible and free from uncertainties such as the mass of the host star. We find that the distribution of period ratios of two exoplanets appears inconsistent with that derived from the Titius-Bode’s relation using the χ2 test. We also found that the distance distribution in exoplanetary systems unlikely follows the uniform distribution or the Poisson’s distribution. It is noted, however, that more rigorous statistical tests should be carried out to reach a more certain conclusion.
提丢斯-波德关系在预测谷神星在太阳系中的位置方面取得了历史上的成功,但它的物理基础仍然是隐藏的。在本研究中,我们试图回答Titius-Bode关系是否普遍适用于具有多个系外行星的系外行星系统的问题。为此,我们统计研究了由一颗恒星承载的32个系外行星系统中两颗行星轨道周期之比的分布。我们只考虑由围绕一颗恒星运行的系外行星得出的周期比,因为所研究的天体尽可能保持简单,并且不受诸如主恒星质量等不确定因素的影响。通过χ2检验,我们发现两颗系外行星的周期比分布与Titius-Bode关系的分布不一致。我们还发现系外行星系统的距离分布不太可能遵循均匀分布或泊松分布。然而,应当指出,为了得出更确定的结论,应当进行更严格的统计检验。
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引用次数: 0
Solar Flux Effects on the Variations of Equatorial Electrojet (EEJ) and Counter-Electrojet (CEJ) Current across the Different Longitudinal Sectors during Low and High Solar Activity 太阳通量对低、高太阳活动期间赤道电喷流(EEJ)和反电喷流(CEJ)在不同纵向扇区上变化的影响
IF 0.5 Q3 Earth and Planetary Sciences Pub Date : 2023-06-01 DOI: 10.5140/jass.2023.40.2.45
A. Cherkos
This study examined the effect of solar flux (F10.7) and sunspots number (R) on the daily variation of equatorial electrojet (EEJ) and morning/afternoon counter electrojet (MCEJ/ACEJ) in the ionospheric E region across the eight longitudinal sectors during quiet days from January 2008 to December 2013. In particular, we focus on both minimum and maximum solar cycle of 24. For this purpose, we have collected a 6-year ground-based magnetic data from multiple stations to investigate EEJ/CEJ climatology in the Peruvian, Brazilian, West & East African, Indian, Southeast Asian, Philippine, and Pacific sectors with the corresponding F10.7 and R data from satellites simultaneously. Our results reveal that the variations of monthly mean EEJ intensities were consistent with the variations of solar flux and sunspot number patterns of a cycle, further indicating that there is a significant seasonal and longitudinal dependence. During the high solar cycle period, F10.7 and R have shown a strong peak around equinoctial months, consequently, the strong daytime EEJs occurred in the Peruvian and Southeast Asian sectors followed by the Philippine regions throughout the years investigated. In those sectors, the correlation between the day Maxima EEJ and F10.7 strengths have a positive value during periods of high solar activity, and they have relatively higher values than the other sectors. A predominance of MCEJ occurrences is observed in the Brazilian (TTB), East African (AAE), and Peruvian (HUA) sectors. We have also observed the CEJ dependence on solar flux with an anti-correlation between ACEJ events and F10.7 are observed especially during a high solar cycle period.
本文研究了2008年1月至2013年12月,太阳通量(F10.7)和太阳黑子数(R)对电离层E区8个纵向扇区赤道电喷流(EEJ)和早晚反电喷流(MCEJ/ACEJ)日变化的影响。我们特别关注最小和最大太阳周期24。为此,我们收集了秘鲁、巴西、西非和东非、印度、东南亚、菲律宾和太平洋扇区6年的地面磁资料,并同时利用相应的卫星F10.7和R数据研究了EEJ/CEJ气候学。结果表明,月平均EEJ强度的变化与一个周期内太阳通量和黑子数的变化趋势一致,具有明显的季节依赖性和纵向依赖性。在太阳活动高周期,F10.7和R在分点月前后出现强烈的峰值,因此,在调查的年份中,强烈的日间eej出现在秘鲁和东南亚地区,其次是菲律宾地区。在这些扇区中,日Maxima EEJ与F10.7强度在太阳活动高峰期呈正相关,且相对高于其他扇区。MCEJ主要发生在巴西(TTB)、东非(AAE)和秘鲁(HUA)地区。我们还观察到CEJ对太阳通量的依赖性,特别是在太阳活动高周期期间,CEJ事件与F10.7呈负相关。
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引用次数: 0
Comment on “Interaction of Ion Cyclotron Electromagnetic Wave with Energetic Particles in the Existence of Alternating Electric Field Using Ring Distribution” by Shukla KN, Kumari J, Pandey RS Shukla KN, Kumari J, Pandey RS对“交变电场存在下离子回旋电磁波与高能粒子的环形相互作用”的评论
IF 0.5 Q3 Earth and Planetary Sciences Pub Date : 2023-06-01 DOI: 10.5140/jass.2023.40.2.89
S. Chandra
It is already discussed categorically and in detail that for the alternating current (AC) electric field parallel to the magnetic field, the dispersion relation is too complicated and cannot be expressed through a simple expression. As they claim to use a simple relation, which cannot be applicable, the results of Shukla et al. (2022) are not reliable. Propagation of waves through a magnetized plasma having AC electric field has been discussed in detail in literature. For propagation of waves in plasma, the dielectric tensor is expressed by Summers et al. (1994), where εij are (nine) elements of dielectric tensor ε, and the wavevector is k = k⊥i ^ + kǁ k ^ , where i ^ and k ^ are, respectively, unit vector along the x-axis and z-axis of Cartesian coordinate system. Let us review our earlier work in brief. We have investigated two cases: (i) the magnetic field is perpendicular to the AC electric field (Chandra & Sharma 2020a), and (ii) the magnetic field is parallel to the AC electric field (Chandra & Sharma 2020b). Chandra & Sharma (2020a) considered the case of AC electric field E0 = E0 sin νt i ^ , and ambient magnetic field B = B0k ^ , i.e., the direction of the electric field is perpendicular to the direction of the magnetic field. For the propagation of wave parallel to the magnetic filed (i.e., along the z-axis), we have k⊥ = 0, kǁ = k, N⊥ = 0 and Nǁ = N. Therefore, ε13 = ε31 = ε23 = ε32 = 0, so that, we have
对于平行于磁场的交流电场,色散关系过于复杂,不能用一个简单的表达式来表示。Shukla et al.(2022)的结果不可靠,因为他们声称使用了一个简单的关系,这是不适用的。已有文献详细讨论了波在具有交流电场的磁化等离子体中的传播。对于波在等离子体中的传播,介质张量由Summers et al.(1994)表示,其中εij是介电张量ε的(9)个元素,波向量为k = k⊥i ^ + kk ^,其中i ^和k ^分别是沿笛卡尔坐标系的x轴和z轴的单位矢量。让我们简单地回顾一下我们以前的工作。我们研究了两种情况:(i)磁场垂直于交流电场(Chandra & Sharma 2020a), (ii)磁场平行于交流电场(Chandra & Sharma 2020b)。Chandra & Sharma (2020a)考虑了交流电场E0 = E0 sin νt i ^,环境磁场B = B0k ^的情况,即电场方向垂直于磁场方向。对于与磁场平行的波的传播(即沿z轴),我们有k⊥= 0,k_ = k, N⊥= 0和n_ = N。因此,ε13 = ε31 = ε23 = ε32 = 0,所以,我们有
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引用次数: 0
Lessons Learned from Korea Pathfinder Lunar Orbiter Flight Dynamics Operations: NASA Deep Space Network Interfaces and Support Levels 从韩国探路者月球轨道飞行器飞行动力学操作中吸取的教训:NASA深空网络接口和支持水平
IF 0.5 Q3 Earth and Planetary Sciences Pub Date : 2023-06-01 DOI: 10.5140/jass.2023.40.2.79
Young-Joo Song, Seung-Su Hong, Dong-Gyu Kim, Jun Bang, Jonghee Bae
On Aug. 4, 2022, at 23:08:48 (UTC), the Korea Pathfinder Lunar Orbiter (KPLO), also known as Danuri, was launched using a SpaceX Falcon 9 launch vehicle. Currently, KPLO is successfully conducting its science mission around the Moon. The National Aeronautics and Space Administration (NASA)’s Deep Space Network (DSN) was utilized for the successful flight operation of KPLO. A great deal of joint effort was made between the Korea Aerospace Research Institute (KARI) and NASA DSN team since the beginning of KPLO ground system design for the success of the mission. The efficient utilization and management of NASA DSN in deep space exploration are critical not only for the spacecraft’s telemetry and command but also for tracking the flight dynamics (FD) operation. In this work, the top-level DSN interface architecture, detailed workflows, DSN support levels, and practical lessons learned from the joint team’s efforts are presented for KPLO’s successful FD operation. Due to the significant joint team’s efforts, KPLO is currently performing its mission smoothly in the lunar mission orbit. Through KPLO cooperative operation experience with DSN, a more reliable and efficient partnership is expected not only for Korea’s own deep space exploration mission but also for the KARI-NASA DSN joint support on other deep space missions in the future.
2022年8月4日23:08:48 (UTC),韩国探路者月球轨道飞行器(KPLO),也被称为达努里,使用SpaceX猎鹰9号运载火箭发射。目前,KPLO正在成功地执行绕月科学任务。美国国家航空航天局(NASA)的深空网络(DSN)被用于KPLO的成功飞行操作。韩国航空宇宙研究院(KARI)和美国宇航局(NASA) DSN团队从KPLO地面系统设计开始,就为此次任务的成功进行了大量的共同努力。深空探测中NASA深空信号网络的有效利用和管理不仅对航天器的遥测和指挥至关重要,而且对飞行动力学(FD)运行的跟踪也至关重要。在这项工作中,提出了顶级DSN接口架构,详细的工作流程,DSN支持级别以及从联合团队的努力中获得的实践经验,以帮助KPLO成功地进行FD操作。由于联合团队的重大努力,KPLO目前正在月球任务轨道上顺利执行任务。通过KPLO与深空网络的合作运营经验,不仅可以为韩国自己的深空探测任务提供更可靠和高效的伙伴关系,而且还可以为karii - nasa深空网络在未来的其他深空任务提供联合支持。
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引用次数: 1
Comparative Analysis of Cosmic Radiation Exposure Dose Due to the Russian Detour Route 俄罗斯绕行路线的宇宙辐射照射剂量比较分析
IF 0.5 Q3 Earth and Planetary Sciences Pub Date : 2023-06-01 DOI: 10.5140/jass.2023.40.2.59
Hee-Bok Ahn, Jaeyoung Kwak, Jung-Lae Hwang
Since the World Health Organization (WHO) officially announced a global pandemic on March 12, 2020, the aviation industry in the world has been experiencing difficulties for a long time. Meanwhile, the Ukraine war broke out in February, and from March 15, domestic airlines must operate air routes bypassing Russian airspace despite the longer flight time. Therefore, as the flight time increases, the cosmic radiation exposure dose of the crew members is also expected to increase. Here we compare the radiation exposure dose between the route doses for the eastern United States and Europe before and after the detour route usage. Through the comparison analysis, we tried to understand how cosmic radiation changes depending on the flight time and the latitude and which one contributes more. We expect that this study can be used for the policy update for the safety management of cosmic radiation for aircrews in Korea.
自2020年3月12日世界卫生组织正式宣布全球大流行以来,世界航空业长期陷入困境。与此同时,2月份乌克兰战争爆发,从3月15日开始,国内航空公司必须绕过俄罗斯领空,尽管飞行时间更长。因此,随着飞行时间的增加,机组人员的宇宙辐射暴露剂量也有望增加。在这里,我们比较了美国东部和欧洲使用绕行路线前后的路线剂量的辐射暴露剂量。通过对比分析,我们试图了解宇宙辐射是如何随着飞行时间和纬度的变化而变化的,以及哪个贡献更大。本研究可为我国机组人员宇宙辐射安全管理政策的更新提供参考。
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引用次数: 0
Observations for the Ionosphere Using European Incoherent Scatter (EISCAT) in the Dayside Polar Cap/Cusp and Auroral Region 利用欧洲非相干散射(EISCAT)在日侧极帽/尖和极光区观测电离层
IF 0.5 Q3 Earth and Planetary Sciences Pub Date : 2023-03-01 DOI: 10.5140/jass.2023.40.1.1
G. Jee, E. Ji, Eunsol Kim, Y. Kwak, Changsup Lee, H. Kwon, Ji-Eun Kim, Young-bae Ham, Ji-Hee Lee, Jeong‐Han Kim, Tae-Yong Yang, H. Kam
Korea Polar Research Institute (KOPRI) and Korea Astronomy and Space Institute (KASI) have been participating in the European Incoherent Scatter (EISCAT) Scientific Association as an affiliate institution in order to observe the polar ionosphere since 2015. During the period of December 16–21, 2016 and January 3–9, 2018, the observations for the polar ionospheric parameters such as the electron density profiles, ion drift, and electron/ion temperature are carried out in the polar cap/cusp region by the EISCAT Svalbard radar (ESR). The purpose of the observations is to investigate the characteristic of the winter ionosphere in the dayside polar cap/cusp region. In this paper, we briefly report the results of the ESR observations for winter daytime ionosphere and also the simultaneous observations for the ionosphere-thermosphere system together with the balloon-borne instrument High-Altitude Interferometer WIND Experiment (HIWIND) performed by the High Altitude Observatory (HAO), National Center for Atmospheric Research (NCAR). We further introduce our research activities using long-term EISCAT observations for the occurrence of ion upflow and the climatology of the polar ionospheric density profiles in comparison with the mid-latitude ionosphere. Finally, our future research plans will briefly be introduced.
韩国极地研究所(KOPRI)和韩国天文空间研究所(KASI)为了观测极地电离层,从2015年开始作为附属机构参加了欧洲非相干散射(EISCAT)科学协会。2016年12月16日至21日和2018年1月3日至9日,利用ESR在极帽/尖区对极地电离层电子密度分布、离子漂移和电子/离子温度等参数进行了观测。观测的目的是研究昼侧极帽/极尖区冬季电离层的特征。本文简要介绍了中国国家大气研究中心(NCAR)高空观测台(HAO)冬季日间电离层ESR观测结果和电离层-热层系统同步观测结果以及气球载仪高空干涉仪风实验(HIWIND)。我们进一步介绍了我们的研究活动,利用长期的EISCAT观测,离子上涌的发生和极地电离层密度剖面的气候学与中纬度电离层的比较。最后简要介绍我们未来的研究计划。
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引用次数: 0
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Journal of Astronomy and Space Sciences
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