Langmuir probe measurements within the discharge channel of the 20-kW NASA-300M and NASA-300MS Hall thrusters /

Bibliographic Details
Main Author:	Shastry, Rohit (Author)
Corporate Author:	United States. National Aeronautics and Space Administration. Science Mission Directorate (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2013.
Series:	NASA technical memorandum ; 2013-216611.
Subjects:	Hall thrusters. Electrostatic probes. Channel capacity. Solar electric propulsion. Magnetic shielding. Plasma potentials.
Online Access:	https://purl.fdlp.gov/GPO/gpo56098 http://purl.fdlp.gov/GPO/gpo56098

Description
Item Description:	Title from title screen (viewed on March 19, 2015). "December 2013." "Prepared for the 33rd International Electric Propulsion Conference (IEPC2013) sponsored by the Aerojet Rocketdyne, et al., Washington, D.C., October 6-10, 2013."
Physical Description:	1 online resource (17 pages) : illustrations.
Bibliography:	Includes bibliographical references (pages 16-17).