Trajectory assessment and optimisation in the context of small launcher design
The paper presents a mathematical model that can be used to quickly define a nominal trajectory for the studied small launcher configuration. The tool developed based on the proposed mathematical model can be used separately for trajectory assessments or it can be integrated in a multidisciplinary o...
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| Principais autores: | , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2020-06-01
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| Series: | INCAS Bulletin |
| Assuntos: | |
| Acceso en liña: | https://bulletin.incas.ro/files/onel__chelaru__vol_12_iss_2.pdf |
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