A perspective on the luminous efficiency approach for meteoroid mass estimation

IF 3.2 2区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS
Icarus Pub Date : 2026-03-15 Epub Date: 2025-12-22 DOI:10.1016/j.icarus.2025.116922
Christopher O. Johnston , Alireza Mazaheri , Eric C. Stern
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引用次数: 0

Abstract

A perspective on the luminous efficiency approach for determining the pre-atmospheric mass of a meteoroid from a measured light-curve is presented for meteors in the continuum flow regime. This perspective interprets the mass-loss rate evaluated from the luminous efficiency approach as a solution to the meteoroid surface energy balance, with the measured light-curve serving as a proxy for the radiative heating to the meteoroid surface. This differs from the standard interpretation that equates the radiation from the light-curve to a change in the kinetic energy of the meteor. Mathematically, the developed perspective is identical to the standard luminous efficiency approach, except that the deceleration term is shown to be extraneous. This perspective provides a clear relationship between the measured light-curve and the mass loss of a meteor, which is based on the observation that the radiative heating that drives the mass loss (through the surface energy balance) also provides the radiation for the light-curve. Furthermore, this perspective provides a simple mathematical framework for interpreting the impact of fragmentation on the luminous efficiency. This framework shows that the luminous efficiency of a fragmented meteoroid is a weighted sum of the luminous efficiency from the various fragments, which may each be assessed based on single-body simulations. To generate these single-body simulations, state-of-the-art flowfield and radiation simulations are performed for meteoroid diameters ranging from 0.02 to 100 m, velocities ranging from 12 to 24 km/s, and altitudes ranging from 20 to 50 km. The luminous efficiency values resulting from these simulations are distilled into a correlation and applied to trajectories resulting from the fragment cloud method. This allows the integral luminous efficiency to be computed using the developed luminous efficiency model and defined fragmentation framework. Both the silicon and visible passbands are considered. For the silicon passband, the computed integral luminous efficiency values track closely with the experimentally derived integral luminous efficiency model developed by Brown et al. (2002). This represents the first theoretical derivation of the integral luminous efficiency approach based on fully coupled radiation and ablation simulations with viscous effects, which also captures the impact of individual meteoroids that are combined using the developed fragmentation framework.
流星体质量估算的发光效率方法研究进展
本文提出了用光曲线测量流星体大气前质量的发光效率方法在连续流状态下的应用。这种观点解释了从发光效率方法评估的质量损失率作为流星体表面能量平衡的解决方案,测量的光曲线作为流星体表面辐射加热的代理。这与将光曲线的辐射等同于流星动能变化的标准解释不同。在数学上,所开发的视角与标准的发光效率方法是相同的,只是减速项被证明是无关的。这种观点提供了测量的光曲线和流星质量损失之间的清晰关系,这是基于观测到的驱动质量损失的辐射加热(通过表面能量平衡)也为光曲线提供了辐射。此外,这一视角为解释碎片化对发光效率的影响提供了一个简单的数学框架。该框架表明,碎片流星体的发光效率是来自不同碎片的发光效率的加权和,每个碎片都可以基于单一物体模拟来评估。为了生成这些单一物体的模拟,最先进的流场和辐射模拟进行了流星体直径范围从0.02到100米,速度范围从12到24公里/秒,高度范围从20到50公里。从这些模拟得到的发光效率值被提炼成一种相关性,并应用于由碎片云方法得到的轨迹。这允许使用开发的发光效率模型和定义的碎片框架来计算积分发光效率。硅通带和可见光通带都被考虑。对于硅通带,计算的积分发光效率值与Brown等人(2002)开发的实验推导的积分发光效率模型密切相关。这代表了基于具有粘性效应的完全耦合辐射和烧蚀模拟的积分发光效率方法的第一个理论推导,该方法还捕获了使用已开发的碎片框架组合的单个流星体的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Icarus
Icarus 地学天文-天文与天体物理
CiteScore
6.30
自引率
18.80%
发文量
356
审稿时长
2-4 weeks
期刊介绍: Icarus is devoted to the publication of original contributions in the field of Solar System studies. Manuscripts reporting the results of new research - observational, experimental, or theoretical - concerning the astronomy, geology, meteorology, physics, chemistry, biology, and other scientific aspects of our Solar System or extrasolar systems are welcome. The journal generally does not publish papers devoted exclusively to the Sun, the Earth, celestial mechanics, meteoritics, or astrophysics. Icarus does not publish papers that provide "improved" versions of Bode''s law, or other numerical relations, without a sound physical basis. Icarus does not publish meeting announcements or general notices. Reviews, historical papers, and manuscripts describing spacecraft instrumentation may be considered, but only with prior approval of the editor. An entire issue of the journal is occasionally devoted to a single subject, usually arising from a conference on the same topic. The language of publication is English. American or British usage is accepted, but not a mixture of these.
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