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Comparison study of exhaust plume impingement effects of small mono- and bipropellant thrusters using parallelized DSMC method
A space propulsion system is important for the normal mission operations of a spacecraft by adjusting its attitude and maneuver. Generally, a mono- and a bipropellant thruster have been mainly used for low thrust liquid rocket engines. But as the plume gas expelled from these small thrusters diffuse...
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
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Public Library of Science
2017
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| Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5479541/ https://www.ncbi.nlm.nih.gov/pubmed/28636625 http://dx.doi.org/10.1371/journal.pone.0179351 |