A high current cathode plasma jet flow model for the Pulsed Plasma Thruster
Shaw, P and Lappas, VJ A high current cathode plasma jet flow model for the Pulsed Plasma Thruster In: 32nd International Electric Propulsion Conference, 2011-09-11 - 2011-09-15, Wiesbaden, Germany.
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Studies with a Pulsed Plasma Thruster have shown that the ratio between the electromagnetic contribution of the impulse bit between a PPT with Teflon™ to when Teflon™ is not present is around 0.6~0.75 over the range of experiments that were conducted. The trade-off in the mass and volume savings compared to a reduced performance meant that a PPT without Teflon™ was developed. A simplified hydrodynamic model using boundary conditions taken from experimental literature from the cathodic arc plasma field was applied to a plasma flow model that took account of pinching effects from the high current plasma. The model was then compared to experimental results to show its validity.
|Item Type:||Conference or Workshop Item (Paper)|
|Additional Information:||Paper presented at the 32nd International Electric Propulsion Conference, Wiesbaden, Germany September 11–15, 2011. Copyright the authors.|
|Divisions:||Faculty of Engineering and Physical Sciences > Electronic Engineering > Surrey Space Centre|
|Depositing User:||Symplectic Elements|
|Date Deposited:||23 Mar 2012 09:51|
|Last Modified:||23 Sep 2013 18:53|
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