Ion Beam Propulsion StudyThe Ion Beam Propulsion Study was a joint high-level study between the Applied Physics Laboratory operated by NASA and ASRC Aerospace at Kennedy Space Center, Florida, and Berkeley Scientific, Berkeley, California. The results were promising and suggested that work should continue if future funding becomes available. The application of ion thrusters for spacecraft propulsion is limited to quite modest ion sources with similarly modest ion beam parameters because of the mass penalty associated with the ion source and its power supply system. Also, the ion source technology has not been able to provide very high-power ion beams. Small ion beam propulsion systems were used with considerable success. Ion propulsion systems brought into practice use an onboard ion source to form an energetic ion beam, typically Xe+ ions, as the propellant. Such systems were used for steering and correction of telecommunication satellites and as the main thruster for the Deep Space 1 demonstration mission. In recent years, "giant" ion sources were developed for the controlled-fusion research effort worldwide, with beam parameters many orders of magnitude greater than the tiny ones of conventional space thruster application. The advent of such huge ion beam sources and the need for advanced propulsion systems for exploration of the solar system suggest a fresh look at ion beam propulsion, now with the giant fusion sources in mind.
Document ID
20090022210
Acquisition Source
Kennedy Space Center
Document Type
Extended Abstract
Date Acquired
August 24, 2013
Publication Date
March 3, 2008
Publication Information
Publication: John F. Kennedy Space Center's Technology Development and Application 2006-2007 Report
IDRelationTitle20090022202Collected WorksJohn F. Kennedy Space Center's Technology Development and Application 2006-2007 Report20090022202Collected WorksJohn F. Kennedy Space Center's Technology Development and Application 2006-2007 Report