MENG ZHAO

Ms. MENG ZHAO

orcid

Research Focus & Metrics

Academic Career Length

3Years (2024-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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16 December 2024 in Acta Astronautica
Verified
Journal Article
Closed access
PSPeng Shu
Peng Shu
MZMENG ZHAO
MENG ZHAO
ZLZhen-Yu Li
Zhen-Yu Li
WSWei Sun
Wei Sun
YLYuqiang Li
Yuqiang Li
YLYa-Zhong Luo
Ya-Zhong Luo

19 December 2024 in arXiv
Verified
Preprint
Open access
PDF file
PSPeng Shu
Peng Shu
MZMENG ZHAO
MENG ZHAO
ZLZhen-Yu Li
Zhen-Yu Li
WSWei Sun
Wei Sun
YLYu-Qiang Li
Yu-Qiang Li
YLYazhong Luo
Yazhong Luo
The increasing population of objects in geostationary orbit has raised concerns about the potential risks posed by debris clouds resulting from fragmentation. The short-term evolution and associated hazards of debris generated by collisions in the geostationary region is investigated in this study. The initial distribution of two debris clouds is modeled using a single probability density function. The combined distribution of the evolved clouds is determined by solving boundary value problems. The risks associated with these debris clouds are evaluated by calculating the instantaneous impact rate and cumulative collision probability. The probability of collisions with millimeter-sized fragments may increase to 1% within 36 hours, while the probability of collisions with fragments 5 cm or larger is approximately $10^{-5}$. These findings underscore the vulnerability of the geostationary region to space traffic accidents.

25 March 2026 in Aerospace
Verified
Journal Article
Open access
PDF file
PSPeng Shu
Peng Shu
MZMENG ZHAO
MENG ZHAO
YWYuyan Wu
Yuyan Wu
ZYZhen Yang
Zhen Yang
YLYuqiang Li
Yuqiang Li
The breakup of Intelsat 33E on 19 October 2024 posed a potential risk to satellites in the Geostationary Earth Orbit (GEO). This study analyzes the evolution and distribution of these fragments using a probabilistic approach. The initial distribution of the fragments, derived from the NASA Standard Breakup Model, indicates the generation of 4393 fragments larger than 1 cm. The spatial propagation of these fragments is modeled analytically in the Earth-Centered Earth-Fixed reference frame, showing the formation of high-density ring structures in the equatorial plane from 24 h to 28 days after the breakup. The orbits of 36 cataloged fragments are retrieved and compared with the probability density. Furthermore, Monte Carlo simulations validate the probabilistic model and highlight its efficiency in capturing low-probability events. Collision risks to other GEO satellites are assessed, showing that the top 10% of satellites encounter a collision probability of up to 10−8 after 28 days. Satellites near the equatorial plane are at higher risk, whereas those with higher inclinations are less affected. These findings underscore the need for enhanced monitoring and mitigation strategies for GEO breakup events, given the challenges in detecting small fragments.