Multimode, high specific Impulse Hall thruster technology

36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2000, Pages

  Butler, G W ^a   Yuen, J L ^a   Tverdokhlebov, S O ^b   Semenkin, A V ^b   Kochergin, A V ^b   Solodukhin, A E ^b   Jankovsky, R S ^c  

^a BOEING COMPANY   (United States)

^b CENTRAL RESEARCH INSTITUTE OF MACHINE BUILDING   (Russian Federation)

^c NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

NASA; PROPULSION;

APPLIED VOLTAGES; HIGH SPECIFIC IMPULSE; MASS FLOW RATE; OPERATIONAL CAPABILITIES; OPERATIONAL PERFORMANCE; PERFORMANCE CAPABILITY; SPECIFIC IMPULSE; THRUSTER WITH ANODE LAYERS;

HALL THRUSTERS;

EID: 84896458838     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Abdukhanov, M. A., et al. "The Study of two-stage TAL performances with different working substances," Abstracts for II All Union Conference on Plasma Accelerators and Ion Injectors (in Russian), 1972. Also Grishin S. D et al. Electric Thrusters, Mashinostroenie, 1975 (in Russian)
2. Tverdokhlebov, S. O., "Study of Double-Stage Anode Layer Thruster Using Inert Gases," IEPC-93-232.
3. Tverdokhlebov, S. O., Garkusha V.I., "High Voltage Mode of TAL Thruster Operation," IEPC-97-023.
4. Jankovsky, R., S. Tverdokhlebov, D. Manzella, "High Power Hall Thrusters," AIAA-99-2949.
5. Semenkin A.V., "External Anode Layer Thruster Parameters at High Specific Impulse Regimes," IEPC-97-055.