Development and characterization of a diverging cusped field thruster and a lanthanum hexaboride hollow cathode
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2008. === MIT Aero Library copy: printed in pages. === Includes bibliographical references (leaves 147-152). === A low power, magnetically confined plasma thruster has been developed and undergone preliminar...
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| Format: | Others |
| Language: | English |
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Massachusetts Institute of Technology
2009
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| Online Access: | http://hdl.handle.net/1721.1/45239 |