INJECTED PROPELLANT IONIZATION IN MPD THRUSTERS

Citation
Rl. Burton et N. Tiliakos, INJECTED PROPELLANT IONIZATION IN MPD THRUSTERS, Journal of propulsion and power, 9(5), 1993, pp. 764-770
Citations number
46
Categorie Soggetti
Aerospace Engineering & Tecnology
ISSN journal
07484658
Volume
9
Issue
5
Year of publication
1993
Pages
764 - 770
Database
ISI
SICI code
0748-4658(1993)9:5<764:IPIIMT>2.0.ZU;2-0
Abstract
A model is presented for the self-magnetized, weakly ionized preioniza tion region at the entrance to a magnetoplasmadynamic (MPD) accelerato r. The model is steady, one-dimensional and inviscid, and assumes supe rsonic flow of argon plasma with zero current in the region. Heavy par ticle temperature is constant, and electron temperature T(e) is determ ined by ambipolar diffusion and by photo- and electron-impact ionizati on processes. The plasma continuity, momentum, and energy equations ar e integrated numerically with appropriate boundary conditions, giving a region width DELTAx ranging from 3 to 17 mm, depending on density, a nd a degree of ionization alpha increasing from an initial value of al pha = 10(-7) to alpha = 4 +/- 2 x 10(-4) at the MPD accelerator inlet. The electron temperature rises monotonically from T(e) = 1000 K to T( e) is-approximately-equal-to 18,000 K, a level sufficient to sustain M PD accelerator operation. The total electrostatic potential across DEL TAx is DELTAV = 12.5 +/- 0.6 V. Reducing the injected particle flux Q0 increases DELTAx, until a critical Q0 is reached below which no solut ions exist.