Numerical Validation of a Pyroshock Test System and Application to Qualification Tests
Spacecraft are exposed to severe mechanical loads, i.e., shock loads, during their journey to orbit. Such loads usually develop due to a separation event through the activation of pyrotechnic devices. They might be transmitted throughout the entire structure and strongly influence the service perfor...
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| Principais autores: | , |
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| Format: | Artigo |
| Sprog: | Inglês |
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MDPI AG
2022-07-01
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| Serier: | Aerospace |
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| Online adgang: | https://www.mdpi.com/2226-4310/9/8/400 |
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