Current theory and experimental data on propellant utilization in electron-bombardment ion thrusters are reviewed. Because the majority of investigations have been conducted with mercury, the presentation emphasizes that propellant. The results are presented in as general a form as possible to facilitate use in areas other than space propulsion.
Maximum propellant utilization in an electron-bombardment thruster.
American Physical Society and Brookhaven National Laboratory, Symposium on Ion Sources and Formation of Ion Beams ; 1971 ; Upton, NY
01.10.1971
Aufsatz (Konferenz)
Keine Angabe
Englisch
Ion-Thruster Propellant Utilization
NTIS | 1971
|Ion-thruster propellant utilization
TIBKAT | 1971
|