The source flow method developed by G.A. Simons for calculating the far field plume density produced by high thrust rocket nozzles is modified and applied to low thrust resistojet nozzles with Reynolds numbers on the order of 4000 to 7000. Simons' original method and the modified analysis are compared to mass flux measurements taken by Chirivella in a JPL vacuum tank facility. Results of the comparison show the modified analysis presented more accurately predicts the mass flux at large angles from the nozzle centerline than Simons' original method. The modified Simons analysis is then used to calculate the plume structure and two contamination parameters, number column density and back flow, for five nozzle geometries representative of Space Station resistojets.
Resistojet Plume and Induced Environment Analysis
1987
60 pages
Report
No indication
English
Rocket Engines & Motors , Space Technology , Environment pollution , Gas density , Resistojet engines , Rocket exhaust , Spacecraft contamination , Spacecraft environments , Flow distribution , Heat transfer , Laminar boundary layer , Pressure gradients , Rocket nozzles , Space stations , Spacecraft propulsion
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