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- W2114379450 abstract "Pressure measurements taken onboard a suborbital spacecraft exhibit non-periodic pulses during attitude control thruster firings. The attitude control system located at the bottom of the conical spacecraft included eight thrusters for pitch, yaw and roll control. The pitch and yaw thrusters delivered 1.245 N thrust while the roll thrusters delivered 3.278 N with impulses that lasted up to 0.03 s. The pressure sensor was housed inside the spacecraft and was connected to the outside with a 0.1-ni long, 0.022-m diameter tube. Pressure pulses appear instantaneously with the firings even for thrusters without a direct line-of-sight with the sensor entrance. Pressure data are superimposed on a background pressure that can be attributed to internal outgassing. Plumes from thrusters with the same level of thrust result in large differences in pressure depending on their orientation with respect to the pressure sensor. Navier Stokes simulations of the thruster nozzle and plume flow are also presented. Data analysis and simulations demonstrate plume wrap-around and free surface/plume interaction phenomena." @default.
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- W2114379450 date "1997-06-23" @default.
- W2114379450 modified "2023-09-27" @default.
- W2114379450 title "Flight data analysis and simulation of attitude control thruster plumes" @default.
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- W2114379450 doi "https://doi.org/10.2514/6.1997-2534" @default.
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