Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Randy L. Spicer"'
Publikováno v:
AIAA Scitech 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::183bab4127a30f0facb3bef03bfdc304
https://doi.org/10.2514/6.2020-1120
https://doi.org/10.2514/6.2020-1120
Publikováno v:
AIAA Scitech 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d016239399589ca04ee49fa4ce80fe4c
https://doi.org/10.2514/6.2020-1668
https://doi.org/10.2514/6.2020-1668
Autor:
Randy L. Spicer, Jonathan Black
Publikováno v:
AIAA Scitech 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8a1caadeee98e2072c37230efe5902d7
https://doi.org/10.2514/6.2020-1432
https://doi.org/10.2514/6.2020-1432
Publikováno v:
50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9ac8779e2a5f8e3de9a2f11f7233d3b5
https://doi.org/10.2514/6.2009-2635
https://doi.org/10.2514/6.2009-2635
The plume of a Busek BHT-200 xenon Hall thruster has been characterized through measurements from various plasma electrostatic probes. Ion current flux, plasma potential, plasma density, and electron temperatures were measured from the near-field plu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::89cd52ffc2bd89a23aabc4ce983cb649
https://doi.org/10.21236/ada473510
https://doi.org/10.21236/ada473510
Publikováno v:
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
The plume of a Busek BHT-200 xenon Hall thruster has been characterized through measurements from various plasma electrostatic probes. Ion current flux, plasma potential, plasma density, and electron temperatures were measured in the near-field of th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::561dd69cfc7928299d52c7c7954f301e
https://doi.org/10.2514/6.2007-5305
https://doi.org/10.2514/6.2007-5305
Publikováno v:
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
This paper investigates the use of Monte Carlo Collision for modeling particle collisions in electric propulsion plumes by comparing numerical simulations with a vacuum tank experiment conducted at the Air Force Research Laboratory. Simulations are c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::82f7c67e17a0e9ad0107ab5bfc597fd2
https://doi.org/10.2514/6.2006-5025
https://doi.org/10.2514/6.2006-5025