Influences of initial voltage and electrode size on propellant surface evolution in a coaxial pulsed plasma thruster
Acta Astronautica
Acta Astronautica ; 222
2024-09-01
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
CHARACTERISTICS OF A COAXIAL PULSED PLASMA THRUSTER USING LIQUID PROPELLANT (AIAA 2016-4847)
British Library Conference Proceedings | 2016
|Performance Characteristics of Liquid Propellant Pulsed Plasma Thruster
British Library Conference Proceedings | 2004
|