2026-09-22T14:06:00Z https://www.ideals.illinois.edu/oai-pmh

oai:www.ideals.illinois.edu:2142/42155 2023-07-11 col_2142_14800 col_2142_5131 com_2142_14799 com_2142_234 com_2142_5130

Miley, George H. Krishnamurthy, Akshata 2013-02-03T19:17:42Z 2013-02-03T19:17:42Z 2015-02-03T11:01:02Z 2012-12 2012-12 2012-12 This present work is focused on the development of an IEC thruster based on the jet mode of operation. Discharge characteristics of the IEC jet mode were studied. Current, thermal power, thermal efficiency and thrust measurements were obtained. As an addition, helicon plasma injection into the IEC was studied, and based on findings suitable recommendations for the development of the helicon-injected IEC thruster were proposed. Item withdrawn by Mark Zulauf (zulauf@illinois.edu) on 2012-12-12T19:32:44Z Item was in collections: University of Illinois Theses & Dissertations (ID: 1) No. of bitstreams: 2 Krishnamurthy_Akshata.docx: 33300209 bytes, checksum: 9d6e0cde6404e09d8ca6ead22afeccf6 (MD5) Krishnamurthy_Akshata.pdf: 3571749 bytes, checksum: ca3a2fd59d2844865d8ca9e685c4dff0 (MD5) Made available in DSpace on 2013-02-03T19:17:42Z (GMT). No. of bitstreams: 3 Akshata_Krishnamurthy.pdf: 3867148 bytes, checksum: 1876f7b7ba07a1e6d9426d031dca2c5d (MD5) Krishnamurthy_Akshata.docx: 33300209 bytes, checksum: 9d6e0cde6404e09d8ca6ead22afeccf6 (MD5) license.txt: 4071 bytes, checksum: bb5d2393ec3592248ae58e607965c8b8 (MD5) Item marked as restricted to the 'UIUC Users [automated]' Group (id=2) by Seth Robbins (srobbins@illinois.edu) on 2013-02-03T19:19:03Z Item is restricted until 2015-02-03T19:18:53Z Restriction data tranferred 2014-07-01T11:11:56-05:00 Original Data Group with Access UIUC Users [automated] Release Date: 2015-02-03 13:18:53 UTC Reason: Author requested U of Illinois access only (OA after 2yrs) in Vireo ETD system U of I Only Restriction Lifted for Item 42102 on 2015-02-03T11:01:02Z. http://hdl.handle.net/2142/42155 en Copyright 2012 Akshata Krishnamurthy Inertial Electrostatic Confinement (IEC) thruster electric propulsion space propulsion Helicon inertial confinement Development and characterization of an inertial electrostatic confinement thruster text Aerospace Engineering 1615 Aerospace Engineering 4048 University of Illinois at Urbana-Champaign Thesis M.S. MS: Aerospace Engr -UIUC 10KS4048MS