Satellite design for demise: Thermal Characterisation in Early Re-entry for Dismantlement Mechanisms

HEINRICH, Stephane

DOI: 10.13009/eucass2017-335
Published: 2017
Container: Not recorded
Publisher: Proceedings of the 7th European Conference for Aeronautics and Space Sciences. Milano, Italy, 3-6 july 2017
Open access: no

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Cite this work

BibTeX

@article{allodium:10.13009/eucass2017-335,
  title = {Satellite design for demise: Thermal Characterisation in Early Re-entry for Dismantlement Mechanisms},
  author = {HEINRICH, Stephane},
  year = {2017},
  doi = {10.13009/eucass2017-335},
  url = {https://doi.org/10.13009/eucass2017-335}
}

RIS

TY  - JOUR
TI  - Satellite design for demise: Thermal Characterisation in Early Re-entry for Dismantlement Mechanisms
AU  - HEINRICH, Stephane
PY  - 2017
DO  - 10.13009/eucass2017-335
UR  - https://doi.org/10.13009/eucass2017-335
ER  -

APA

Stephane, H. (2017). Satellite design for demise: Thermal Characterisation in Early Re-entry for Dismantlement Mechanisms. https://doi.org/10.13009/eucass2017-335

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datacite · retrieved 2026-09-26T20:45:33.498Z