@inproceedings{75d79e95fa72459f985690e997bd0265,
title = "Ion energy measurements in a direct wave-drive thruster",
abstract = "An experiment designed to demonstrate ion acceleration in a DirectWave-Drive Thruster (DWDT) was constructed. A DWDT is a new propulsion concept that relies on waves to transfer momentum directly to a plasma without electrodes. In order to demonstrate the existence of accelerated ions, the ion energy distribution function in the plume was mea- sured with a retarding potential analyzer (RPA) for varying powers delivered to the wave launching antenna. For antenna powers up to 700 W, the number of higher energy ions in the distribution function increases, which is consistent with ion acceleration. In order to rule out any spurious effects from the RPA, an insulating plate was placed in front of the RPA, which reduced the number high energy ions in the measured distribution func-tions. The measured increase in the high energy tail of the ion energy distribution function provides evidence for part of a proof-of-concept experiment of the DWDT.",
author = "Feldman, {Matthew S.} and Choueiriy, {Edgar Y.} and Jornsz, {Benjamin A.}",
note = "Publisher Copyright: {\textcopyright} 2015, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; 51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015 ; Conference date: 27-07-2015 Through 29-07-2015",
year = "2015",
doi = "10.2514/6.2015-3726",
language = "English (US)",
isbn = "9781624103216",
series = "51st AIAA/SAE/ASEE Joint Propulsion Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "51st AIAA/SAE/ASEE Joint Propulsion Conference",
}