Numerical Simulation of a Plasma Plume Exhaust from an Electrothermal Plasma Thruster

Autor:	Vasyl M. Rashkovan, Leonid Bazyma
Rok vydání:	2005
Předmět:	Propellant Materials science Computer simulation Mechanical Engineering Aerospace Engineering Plasma Mechanics Plume Fuel Technology Space and Planetary Science Gas constant Direct simulation Monte Carlo Conservation of mass Magnetoplasmadynamic thruster
Zdroj:	Journal of Propulsion and Power. 21:378-382
ISSN:	1533-3876 0748-4658
DOI:	10.2514/1.11337
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::7fab3a58ff557ffc6324a8004b78ef06 https://doi.org/10.2514/1.11337 Zobrazit plný text záznamu