Satellite design for demise thermal characterisation in early re-entry for dismantlement mechanisms-Reference-Cited by-同舟云学术

Satellite design for demise thermal characterisation in early re-entry for dismantlement mechanisms

Published:2019-05 Issue: Volume:158 Page:161-171
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Heinrich Stéphane,Martin Joel,Pouzin Julien

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference19 articles.

1. Space Debris: Models and Risk Analysis;Klinkrad,2006

2. A safer space for a safer world;Johnson,2011

3. Clean Space Implementation Plan;ESA Clean Space Team,2015

4. D4D final Presentation, Thales Presentation at ESTEC, 2-3 February 2016. http://emits.sso.esa.int/emitsdoc/ESTEC/AO8632_RD3-D4D-TASFinalPresentation_forExternalUse.pdf.

5. D4D final Presentation, Airbus Presentation at ESTEC 2-3, February 2016, D4D-PS-ADSS-SY-10000128264. http://emits.sso.esa.int/emitsdoc/ESTEC/AO8632_RD2-D4D-PSADSS-SY-10000128264D4D.pdf.

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Incremental model predictive control for satellite de-orbiting based on drag modulation;Acta Astronautica;2024-02

2. Advancing spacecraft demisability through a novel composite bolt joint system: a step toward sustainable and safe space environments;CEAS Space Journal;2023-12-14

3. A numerical approach to evaluate temperature-dependent peridynamics damage model for destructive atmospheric entry of spacecraft;The Aeronautical Journal;2022-07-28

4. Demisability assessment of space materials;CEAS Space Journal;2022-05-02

5. Development of a frequency-dependent constitutive model for hysteresis of shape memory alloys;Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications;2020-10-06