Performances Study of a Hybrid Rocket Engine
This paper presents a study which analyses the functioning and performances optimization of a hybrid rocket engine based on gaseous oxygen and polybutadiene polymer (HTPB). Calculations were performed with NASA CEA software in order to obtain the parameters resulted following the combustion process....
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| Format: | Article |
| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2018-06-01
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| Series: | INCAS Bulletin |
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| Online Access: | http://bulletin.incas.ro/files/buturache__vol_10_iss_2.pdf |