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Numerical comparison of exhaust plume flow behaviors of small monopropellant and bipropellant thrusters
In general, a space propulsion system has a crucial role in the normal mission operations of a spacecraft. Depending on the types and number of propellants, a monopropellant and a bipropellant thrusters are mostly utilized for low thrust liquid rocket engines. As the plume gas flow exhausted from th...
Autor principal: | Lee, Kyun Ho |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
Public Library of Science
2017
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Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5421759/ https://www.ncbi.nlm.nih.gov/pubmed/28481892 http://dx.doi.org/10.1371/journal.pone.0176423 |
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