Andrenucci, M.; Lensi, R.; Melli, R.; Naso, Vincenzo Criteri di progettazione dei propulsori MDP ad ablazione. (Italian) Zbl 0488.76126 Aerotec. Missili Spazio 59, 322-330 (1980). Page: −5 −4 −3 −2 −1 ±0 +1 +2 +3 +4 +5 Show Scanned Page MSC: 76X05 Ionized gas flow in electromagnetic fields; plasmic flow 78A55 Technical applications of optics and electromagnetic theory 85A99 Astronomy and astrophysics 76W05 Magnetohydrodynamics and electrohydrodynamics Keywords:pulsed plasma thrusters; ablative mass feeding; propulsion of artificial satellites; quasi-steady magnetoplasmadynamic thruster PDFBibTeX XMLCite \textit{M. Andrenucci} et al., Aerotec. Missili Spazio 59, 322--330 (1980; Zbl 0488.76126)