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- W1966236119 abstract "A numerical code has been successfully developed for the investigation of thruster performance using a laser-sustained hydrogen plasma as the propellant. The plasma was sustained using a 10.6-micron CO2 laser beam focused at different positions within the thruster. The physical model assumed that plasma is in thermodynamical equilibrium (LTE), and geometric ray tracing was adopted to describe the laser beam. The steady-state, axisymmetric, Navier-Stokes equations coupled with the laser power absorption process have been solved numerically. A pressure based Navier-Stokes numerical solver using body-fitted coordinates was used to calculate the laser-supported rocket flow which includes both subsonic and supersonic flow regions. From the limited parametric study, which did not try to optimize the rocket performance, it was found that better performance was obtained when the laser beam was focused closer to the rocket throat." @default.
- W1966236119 created "2016-06-24" @default.
- W1966236119 creator A5014013803 @default.
- W1966236119 creator A5046103323 @default.
- W1966236119 date "1987-03-24" @default.
- W1966236119 modified "2023-10-16" @default.
- W1966236119 title "A theoretical investigation of laser-sustained plasma thruster" @default.
- W1966236119 cites W1974115319 @default.
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- W1966236119 doi "https://doi.org/10.2514/6.1987-383" @default.
- W1966236119 hasPublicationYear "1987" @default.
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