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| ISSO Y2004 Annual Report | Contents Investigation
of Plasma Flow Characteristics in a Magneto-Plasma Rocket / 132-133 Abstract--Scientists at NASA-JSC have been engaged in the development of a new space engine concept, designed to propel space vehicles by ionizing and heating neutral gas to high temperatures and then guiding them out of a magnetic nozzle to produce thrust. Research and production will see the development of the VASIMIR (Variable Specific Impulse Magneto-Plasma Rocket. Much like a chemical rocket engine, this engine will transport vehicles faster and allow space travel at greater distances. In 2004, VASIMIR leadership received applications and interviewed potential applicants for a postdoctoral position on the team. A candidate has been selected and has received a letter inviting him to join NASA scientists in this project. He was expected to have begun his research with NASA scientists the first week of April 2005.
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