Debris falling forecast method for spacecraft disintegrating separation-Reference-Cited by-同舟云学术

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Debris falling forecast method for spacecraft disintegrating separation

Published:2023-10-26 Issue:4 Volume:7 Page:455-463
ISSN:2522-008X
Container-title:Astrodynamics
language:en
Short-container-title:Astrodyn

Author:

Li Dun,Li Zhi-Hui,He Yue-Long,Chu Jing-Jiang,Jiang Yu

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42064-023-0177-1.pdf

Reference21 articles.

1. Reyhanoglu, M., Alvarado, J. Estimation of debris dispersion due to a space vehicle breakup during reentry. Acta Astronautica, 2013, 86: 211–218.

2. Balakrishnan, D., Kurian, J. Material thermal degradation under reentry aerodynamic heating. Journal of Spacecraft and Rockets, 2014, 51(4): 1319–1328.

3. Wu, Z., Hu, R., Qu, X., Wang, X., Wu, Z. Space debris reentry analysis methods and tools. Chinese Journal of Aeronautics, 2011, 24(4): 387–395.

4. Caggiano, A., Etse, G. Coupled thermo-mechanical interface model for concrete failure analysis under high temperature. Computer Methods in Applied Mechanics and Engineering, 2015, 289: 498–516.

5. Li, Z., Ma, Q., Cui, J. Finite element algorithm for dynamic thermoelasticity coupling problems and application to transient response of structure with strong aerothermodynamic environment. Communications in Computational Physics, 2016, 20(3): 773–810.

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