Investigation of sandwich shells modelling in order to simulate with robustness the mechanical behaviour of the launchers upper part structures
This paper presents the development of a finite-element model used to study the separation of a launcher payload fairing. This work has been carried out at the French National Space Agency (CNES). In order to capture the complex behaviour of sandwich structures used on the fairing, different methods...
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| Format: | Others |
| Language: | English |
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KTH, Lättkonstruktioner
2017
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-223319 |