Re-entry safety: Analysis and plasma wind tunnel testing of spacecraft design solutions to reduce on-ground casualty risk-Reference-Cited by-同舟云学术

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Re-entry safety: Analysis and plasma wind tunnel testing of spacecraft design solutions to reduce on-ground casualty risk

Published:2023-12 Issue: Volume: Page:
ISSN:2468-8967
Container-title:Journal of Space Safety Engineering
language:en
Short-container-title:Journal of Space Safety Engineering

Author:

Suriani Lucia,Caiazzo Antonio,Ganzer Britta,Lips Tobias,Laurenti Patrice,Lockett Bradley,Schleutker Thorn^ORCID,Soares Tiago,Beck James

Funder

European Space Agency

Publisher

Elsevier BV

Subject

Safety, Risk, Reliability and Quality,Aerospace Engineering

Reference25 articles.

1. ISO 24113:2019 Space systems – Space debris Mitigation Requirements,2019

2. European Space Agency. 2019. ECSS-U-AS-10C Rev.1 – adoption notice of ISO 24113: space systems – space debris mitigation requirements.

3. European Space Agency. 2017. ESSB-ST-U-004, ESA Re-entry safety requirements.

4. Cattani, B.M., Caiazzo, A., Lemmens, S., Innocenti, L., 2021. An overview of design for demise technologies. Presented at the 8th European Conference on Space Debris.

5. D4DBB Team. 2019. D4DBB-OHB-FR-001, Issue 1. D4D breadboarding – TN11 final report.

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