Improved ion containment using a ring-cusp ion thruster
- 1 September 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 21 (5) , 488-495
- https://doi.org/10.2514/3.25684
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Operation of the J-series thruster using inert gasPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Performance of a Magnetic Multipole Line-Cusp Argon Ion ThrusterJournal of Spacecraft and Rockets, 1982
- Magnetoelectrostatic Thruster Physical Geometry TestsJournal of Spacecraft and Rockets, 1982
- Increased capabilities of the 30-cm diameter Hg ion thrusterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- IBIS: A hollow-cathode multipole boundary ion sourceApplied Physics Letters, 1978
- Sensitivity of 30-cm mercury bombardment ion thruster characteristics to accelerator grid designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Cusped Magnetic Field Mercury Ion ThrusterJournal of Spacecraft and Rockets, 1977
- An experimental investigation of multiple ion processes in mercury bombardment thrustersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Measurement of double charged ions in the beam of a 30-cm mercury bombardment thrusterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Magneto-electrostatically contained plasma ion thrusterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969