A Reliable Method for Predicting the Specific Impulse of Chemical Propellants
The specific impulse (Isp) is an important performance parameter that describes energy efficiency of propellant combustion and is intimately related to the rocket engine thrust. In this study, it was possible by using only two variables, i.e., the heat of reaction (Q) and the number of moles of gase...
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| Autor Principal: | |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado: |
Instituto de Aeronáutica e Espaço (IAE)
2018-07-01
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| Series: | Journal of Aerospace Technology and Management |
| Assuntos: | |
| Acceso en liña: | https://www.jatm.com.br/jatm/article/view/945 |
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