2017 8th International Conference on Mechanical and Aerospace Engineering (ICMAE) 2017
DOI: 10.1109/icmae.2017.8038659
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Influence of deflector on impact properties of multi-nozzle LOX/kerosene engine exhaust plume

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“…The development of manned spaceflight, manned lunar landings, Mars exploration, and other major space activities requires the support of advanced rocket engines. According to the development trend for liquid propellant rocket engines [1][2][3], large-thrust liquid oxygen/kerosene engines and heavy carrier rockets will be the major design goals for the future. However, due to the increase in propellant flow rate and the influence of extreme heat flow, it is inevitable that pipeline resistance will increase greatly and that pump load will be large.…”
Section: Introductionmentioning
confidence: 99%
“…The development of manned spaceflight, manned lunar landings, Mars exploration, and other major space activities requires the support of advanced rocket engines. According to the development trend for liquid propellant rocket engines [1][2][3], large-thrust liquid oxygen/kerosene engines and heavy carrier rockets will be the major design goals for the future. However, due to the increase in propellant flow rate and the influence of extreme heat flow, it is inevitable that pipeline resistance will increase greatly and that pump load will be large.…”
Section: Introductionmentioning
confidence: 99%