Sensitivity analysis of spacecraft in micrometeoroids and orbital debris environment based on panel method
2021 · Defence Technology · 15 citations
https://doi.org/10.1016/j.dt.2021.11.001
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Runqiang Chi
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14
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Runqiang Chi is an academic researcher from Harbin Institute of Technology. The author has contributed to research in topics: High-Velocity Impact and Material Behavior & Structural Response to Dynamic Loads & Electromagnetic Launch and Propulsion Technology. The author has an h-index of 14, co-authored 56 publications.
ORCID: 0000-0002-9179-4146Papers by this author
worksDamage analysis of aluminum projectiles and aluminosilicate fibrous porous ceramic targets in hypervelocity impacts
2025 · Advances in Space Research · 3 citations
https://doi.org/10.1016/j.asr.2025.04.016
The effect of projectile nose shape on the formation and expansion of impact-induced ejecta for sand target
2024 · Acta Astronautica · 2 citations
https://doi.org/10.1016/j.actaastro.2024.08.037
An impact sensitivity assessment method of spacecraft based on virtual exterior wall
2023 · Defence Technology · 0 citations
https://doi.org/10.1016/j.dt.2023.02.026
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