Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Aerospace Engineering
Reference22 articles.
1. Kuiper, W., Drolshagen, G., Noomen, R.: Micro-meteoroids and space debris impact risk assessment for the ConeXpress satellite using ESABASE2/Debris. Adv. Space Res. 45, 683–689 (2010). https://doi.org/10.1016/j.asr.2009.10.020
2. Grassi, L., Tiboldo, F., Destefanis, R., Donath, T., Winterboer, A., Evans, L., Janovsky, R., Kempf, S., Rudolph, M., Schäfer, F., Gelhaus, J.: Satellite vulnerability to space debris—an improved 3D risk assessment methodology. Acta Astronaut. 99, 283–291 (2014). https://doi.org/10.1016/j.actaastro.2014.02.006
3. Kelley, R.L.: Using the design for demise philosophy to reduce casualty risk due to reentering spacecraft. In: 63rd International Astronautical Congress (2012)
4. Waswa, P.M.B., Elliot, M., Hoffman, J.A.: Spacecraft design-for-demise implementation strategy & decision-making methodology for low earth orbit missions. Adv. Space Res. 51, 1627–1637 (2013). https://doi.org/10.1016/j.asr.2012.11.020
5. Trisolini, M., Lewis, H.G., Colombo, C.: Survivability and demise criteria for sustainable spacecraft design. In: Proceedings of International Astronautical Congress IAC, pp. 2505–2523 (2015)
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