Ion Detachment in the Helicon Double-Layer Thruster Exhaust Beam
This study is devoted to simulating the orbits of the ions in the supersonic beam observed experimentally in the laboratory development of the helicon double-layer thruster. Given the cylindrical symmetry of the problem, the particle orbits are generated
|Collections||ANU Research Publications|
|Source:||Journal of Propulsion and Power|
|01_Gesto_Ion_Detachment_in_the_Helicon_2006.pdf||145.14 kB||Adobe PDF||Request a copy|
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