Impulse and Performance Measurements of Electric Solid Propellant in a Laboratory Electrothermal Ablation-Fed Pulsed Plasma Thruster

Electric solid propellants are advanced solid chemical rocket propellants that can be controlled (ignited, throttled and extinguished) through the application and removal of an electric current. This behavior may enable the propellant to be used in multimode propulsion systems utilizing the ablative...

Descripción completa

Detalles Bibliográficos

Autores principales:	Matthew S. Glascock, Joshua L. Rovey, Kurt A. Polzin
Formato:	Artigo
Lenguaje:	Inglês
Publicado:	MDPI AG 2020-05-01
Colección:	Aerospace
Materias:	electric solid propellant pulsed plasma thruster electrothermal propulsion ablation-fed arc inverted pendulum thrust stand impulse measurement
Acceso en línea:	https://www.mdpi.com/2226-4310/7/6/70
Etiquetas:	Agregar Etiqueta Sin Etiquetas, Sea el primero en etiquetar este registro!