The VHITAL Program to Demonstrate the Performance and Lifetime of a Bismuth-Fueled Very High Isp Hall Thruster

In the Very High Isp Thruster with Anode Layer (VHITAL) Program the performance, plume and lifetime capability of the radiatively-cooled two stage, bismuth-fueled VHITAL-160 will be characterized in the US and Russia.

[1]  Thomas W. Haag,et al.  Thrust stand for high‐power electric propulsion devices , 1989 .

[2]  G. Berden,et al.  Cavity ring-down spectroscopy: Experimental schemes and applications , 2000 .

[3]  A. Semenkin,et al.  Bismuth propellant option for very high power TAL thruster , 2002 .

[4]  M. Keidar,et al.  Modeling of a high-power thruster with anode layer , 2004 .

[5]  S. George,et al.  Hyperfine-structure measurements in bismuth using a Fourier-transform spectrometer , 1985 .

[6]  A. Yalin,et al.  Detection of sputtered metals with cavity ring-down spectroscopy. , 2005, Applied optics.

[7]  Daniel E. Hastings,et al.  Modeling of Stationary Plasma Thruster-100 Thruster Plumes and Implications for Satellite Design , 1999 .

[8]  Iain D. Boyd,et al.  Computation of the Plume of an Anode-Layer Hall Thruster , 2000 .

[9]  G. Meijer,et al.  Cavity Ringdown Spectroscopy , 1998, Technical Digest. 1998 EQEC. European Quantum Electronics Conference (Cat. No.98TH8326).

[10]  P. Sioshansi,et al.  Surface layer activation technique for monitoring and in-situ wear measurement of turbine components , 1984 .

[11]  Glenn M. Wahlgren,et al.  The laboratory analysis of Bi II and its application to the Bi-rich HgMn star HR 7775 , 2002 .

[12]  Douglas I. Fiehler,et al.  Electric Propulsion System Modeling for the Proposed Prometheus 1 Mission , 2005 .

[13]  Paul J. Wilbur,et al.  Sputter erosion measurements of titanium and molybdenum by cavity ring-down spectroscopy , 2004 .

[14]  Robert S. Jankovsky,et al.  High Voltage SPT Performance , 2001 .

[15]  Iain D. Boyd,et al.  A Review of Spacecraft Material Sputtering By Hall Thruster Plumes , 2001 .

[16]  Ioannis G. Mikellides,et al.  A Hall effect thruster plume model including large-angle elastic scattering , 2001 .

[17]  M. Keidar,et al.  Plasma flow and plasma–wall transition in Hall thruster channel , 2001 .

[18]  Iain D. Boyd,et al.  Review of Hall Thruster Plume Modeling , 2001 .

[19]  Vicky Philipsen,et al.  Influence of the atomic structure on the quantum state of sputtered Ir atoms , 2004 .

[20]  D. J. Kerrisk,et al.  A zero gravity mercury propellant feed system. , 1966 .

[21]  J. Polk.  Characterization of cathode keeper wear by surface layer activation , 2004 .

[22]  Vicky Philipsen,et al.  Sputtering of Ag atoms into metastable excited states , 2002 .

[23]  Iain D. Boyd.  Hall thruster far field plume modeling and comparison to express flight data , 2002 .

[24]  Iain D. Boyd,et al.  3D Simulation of Plume Flows from a Cluster of Plasma Thrusters , 2005 .

[25]  T. W. Conlon.  Doping surfaces with radioactive atoms—for research and industry , 1982 .