Zobrazeno 1 - 10
of 62
pro vyhledávání: '"Thomas W. Haag"'
Autor:
Sarah E. Cusson, Thomas W. Haag, James H. Gilland, Scott J. Hall, Jonathan A. Mackey, Benjamin Jorns, Alec D. Gallimore, Hani Kamhawi, Matthew J. Baird, Peter Y. Peterson
Publikováno v:
Journal of Propulsion and Power. 38:40-50
The performance of a three-channel, 100-kW nested Hall thruster was evaluated on xenon propellant for total powers up to 102 kW. The thruster demonstrated stable operation in all seven available ch...
Publikováno v:
Journal of Propulsion and Power. 36:668-676
The performance of many Hall thrusters has been shown to exhibit sensitivity to background pressure in ground-based test facilities, and this property can have an impact on the prediction of in-spa...
Autor:
Jason D. Frieman, Hani Kamhawi, Jon Mackey, Thomas W. Haag, Peter Y. Peterson, Richard R. Hofer
Publikováno v:
AIAA SCITECH 2022 Forum.
Autor:
Scott King, Anthony Pancotti, James E. Polk, Joseph Blakely, John Ziemer, Mitchell L. R. Walker, Thomas W. Haag
Publikováno v:
J Propuls Power
Accurate, direct measurement of thrust or impulse is one of the most critical elements of electric thruster characterization, and one of the most difficult measurements to make. This paper summarizes recommended practices for the design, calibration,
Autor:
Zachary Taillefer, Lawrence Byrne, T.K. Gray, Thomas W. Haag, Samuel Sawyer, Terry Yu, Dean P. Petters, George Kolencik, Jon Mackey, Vlad Hruby, Mike Strain, Surjeet Paintal, James Szabo
Publikováno v:
AIAA Propulsion and Energy 2020 Forum.
Publikováno v:
Krejci
The characterization of a miniaturized ionic liquid electrospray thruster for nanosatellite applications is presented. The thruster investigated features an emitter array of 480 emitter tips per square centimeter and a 1 cm[superscript 3] propellant
Autor:
Peter Y. Peterson, Hani Kamhawi, Daniel A. Herman, Jonathan A. Mackey, James H. Gilland, Thomas W. Haag, Richard R. Hofer, Jason D. Frieman
Publikováno v:
AIAA Propulsion and Energy 2019 Forum.
The NASA Hall Effect Rocket with Magnetic Shielding (HERMeS) 12.5-kW Hall thruster has been the subject of extensive technology maturation by NASA GRC and JPL in preparation for development into a flight propulsion system. As part of this effort, a s
Publikováno v:
2018 Joint Propulsion Conference.
This paper reviews recent iodine electric propulsion research and development activities at the NASA Glenn Research Center (GRC). Activities included (i) investigation of the iodine compatibility of BaO-CaO-Al2O3 impregnated tungsten hollow cathodes
Publikováno v:
2018 Joint Propulsion Conference.
Autor:
Drew M. Ahern, James H. Gilland, Jason D. Frieman, Thomas W. Haag, Hani Kamhawi, Jonathan A. Mackey, Richard R. Hofer, Peter Y. Peterson, Daniel A. Herman, Wensheng Huang, George J. Williams
Publikováno v:
2018 Joint Propulsion Conference.
The design of a new diagnostic to measure the net erosion of Hall thruster surfaces is presented. This diagnostic consists of a pair of optical non-contact profilometer pens mounted to a set of motion stages, which can interrogate the surface feature