Background Flow Model Validation with a Six-Kilowatt Hall Effect Thruster

Autor:	Jason D. Frieman, Mitchell L. R. Walker, Thomas M. Liu
Rok vydání:	2020
Předmět:	Propellant Materials science business.industry Mechanical Engineering Aerospace Engineering Thrust efficiency Model validation Hall effect thruster High Power Electric Propulsion Fuel Technology Space and Planetary Science Mass flow rate Aerospace engineering business Background flow
Zdroj:	Journal of Propulsion and Power. 36:308-311
ISSN:	1533-3876
DOI:	10.2514/1.b37512
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::29a5c9f6d969f920cdf561f57aff977a https://doi.org/10.2514/1.b37512 Zobrazit plný text záznamu