Parametric analysis of a two-stage small launcher using a MDO approach
The paper presents the influence of the main design requirements on the optimal two-stage small launcher configuration. The influence of target orbit altitude, payload mass, typical missions, and the type of liquid propellant (oxidizer - fuel pair) used on the launcher characteristics is quantified....
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| Principais autores: | , |
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| Format: | Artigo |
| Sprog: | Inglês |
| Udgivet: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2022-03-01
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| Serier: | INCAS Bulletin |
| Fag: | |
| Online adgang: | https://bulletin.incas.ro/files/onel__chelaru__vol_14_iss_1.pdf |
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