Ion velocity measurements in a linear hall thruster

41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2005, Pages

  Gascon, Nicolas ^a,c   Cappelli, Mark A ^a,c   Hargus Jr , William A ^b,d  

^a STANFORD UNIVERSITY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c MC 3032   (United States)

^d Spacecraft Propulsion Branch ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DENSITY OF GASES; EXCITED STATES; HALL THRUSTERS; IONIZATION OF GASES; IONS; OIL FIELD EQUIPMENT; PROPULSION;

HALL DISCHARGE; HIGH SENSITIVITY; HIGH-VACUUM ENVIRONMENTS; ION VELOCITY MEASUREMENT; IONIC TRANSITION; LASER INDUCED FLUORESCENCE; MAGNETIC-FIELD INTENSITY; PROPELLANT VELOCITY;

VELOCITY;

EID: 85088337183     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-4401     Document Type: Conference Paper

References (8)

1. Zhurin V. V., and Kaufman H. R., "Physics of Closed Drift Thrusters" Plasma Sources Sci. Technology 8, pp. R1-R20, 1999.
2. th Joint Propulsion Conference, Cleveland, OH. American Institute of Aeronautics and Astronautics, Washington, DC, 1998. A1AA-98-3336. 3 Schmidt D. P., Meezan N.B., Hargus W.A., Jr., and Cappelli M.A., "A Low-Power, Linear-Geometry Hall Plasma Source with an Open Electron-Drift," Plasma Sources Science and Technology 9, pp. 68-76, 2000.
3. th Joint Propulsion Conference, Salt Lake City, UT, American Institute of Aeronautics and Astronautics, 2001. A1AA-2001-3503.
4. th International Electric Propulsion Conference, Pasadena, CA. Electric Rocket Propulsion Society, 2001. IEPC-01-39.
5. th AIAAIASEE/ASME Joint Propulsion Conference, Huntsville, Alabama. American Institute of Aeronautics and Astronautics, Washington, DC, 2003. A1AA-2003-5156.
6. th AIAAIASEE/ASME Joint Propulsion Conference, Huntsville, Alabama. American Institute of Aeronautics and Astronautics, Washington, DC, 2003. AIAA-2003-5154
7. Bareilles J., Hagelaar G. J. M., Garrigues L., Boniface C., Boeuf J. P. and Gascon N., "Critical Assessment of a TwoDimensional Hybrid Hall Thruster Model: Comparisons with Experiments", Physics of Plasmas Vol. 11, No 6, pp. 3035-3046, 2004.
8. Barral, S., Makowski, K., Peradzynski, Z., Gascon, N., and Dudeck, M., "Wall Material Effects in Stationary Plasma Thrusters II: Near-Wall and Inner-Wall Conductivity," Physics of Plasmas, Vol. 10, No. 10, Oct. 2003, p. 4137.