Accession Number : ADA185674
Title : Completely Magnetically Contained Electrothermal Thrusters.
Descriptive Note : Final technical rept. Sep 84-Aug 85,
Corporate Author : SEITEC INC CLEVELAND OH
Personal Author(s) : Seikel, George R ; Franks, Clifford V
PDF Url : ADA185674
Report Date : 05 Jul 1987
Pagination or Media Count : 47
Abstract : Conceptual designs of potentially attractive high-performance thrusters are defined. These are a kw steady-state radiation-cooled DC thruster and a MW quasi-steady DC thruster. These thrusters offer the potential for long operating life with low erosion rates and 50 to 100% improvements in performance over prior plasma thrusters. The kw thruster would be a prototype of a radiation-cooled electric thruster for future electric propulsion missions. The MW thruster would be an inexpensive experiment to define the potential of subsequent very-high power, steady-state thrusters which would utilize superconducting magnets. The kw thruster would use xenon propellent and the MW thruster would use argon propellent. Both should operate at efficiencies of 50 to 80% in the 2500 to 3000 second specific impulse range. Keywords include: Electric propulsion; Plasma, Electrothermal, and MPD thrusters.
Descriptors : *THRUSTERS, *ELECTRIC PROPULSION, COOLING, DIRECT CURRENT, ELECTRIC PROPULSION, EROSION, LOW RATE, MAGNETS, PERFORMANCE(ENGINEERING), PLASMA ENGINES, RADIATION, STEADY STATE, SUPERCONDUCTORS, XENON, ARGON, MAGNETIC FIELDS, CONTAINMENT(GENERAL), MAGNETOHYDRODYNAMICS
Subject Categories : Electric and Ion Propulsion
Distribution Statement : APPROVED FOR PUBLIC RELEASE