Bare Electrodynamic Tether Ground Simulations in a Dense, High-Speed Plasma Flow
暂无分享,去创建一个
[1] C. Bonifazi,et al. The TSS‐1R Mission: Overview and scientific context , 1998 .
[2] R. D. Estes,et al. Cylindrical Langmuir probes beyond the orbital-motion-limited regime , 2000 .
[3] Alec D. Gallimore,et al. Near- and far-field plume studies of a one-kilowatt arcjet , 1996 .
[4] Robert Forward,et al. Failsafe multistrand tether structures for space propulsion , 1992 .
[5] A. Gallimore,et al. Resonance-probe measurements of plasma densities in electric-propulsion plumes , 1999 .
[6] Jean-Pierre Lebreton,et al. The current‐voltage characteristics of a large probe in low Earth orbit: TSS‐1R results , 1998 .
[7] Gregory G. Spanjers,et al. Performance characteristics of a 5 kW laboratory hall thruster , 1998 .
[8] I. Katz,et al. Observations of ionosphere heating in the TSS‐1 subsatellite presheath , 1994 .
[9] R. D. Estes,et al. The orbital-motion-limited regime of cylindrical Langmuir probes , 1999 .
[10] Les Johnson,et al. Propulsive Small Expendable Deployer System (ProSEDS) space experiment , 1998 .
[11] Eduardo Ahedo,et al. Bare wire anodes for electrodynamic tethers , 1993 .
[12] W. Seifert,et al. Analytical density correction for cylindrical Langmuir probes showing end effects , 1985 .