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Plasmoid Thruster for High Specific-Impulse PropulsionA report discusses a new multi-turn, multi-lead design for the first generation PT-1 (Plasmoid Thruster) that produces thrust by expelling plasmas with embedded magnetic fields (plasmoids) at high velocities. This thruster is completely electrodeless, capable of using in-situ resources, and offers efficiencies as high as 70 percent at a specific impulse, I(sub sp), of up to 8,000 s. This unit consists of drive and bias coils wound around a ceramic form, and the capacitor bank and switches are an integral part of the assembly. Multiple thrusters may be gauged to inductively recapture unused energy to boost efficiency and to increase the repetition rate, which, in turn increases the average thrust of the system. The thruster assembly can use storable propellants such as H2O, ammonia, and NO, among others. Any available propellant gases can be used to produce an I(sub sp) in the range of 2,000 to 8,000 s with a single-stage thruster. These capabilities will allow the transport of greater payloads to outer planets, especially in the case of an I(sub sp) greater than 6,000 s.
Document ID
20100011166
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Fimognari, Peter
(Alabama Univ. Huntsville, AL, United States)
Eskridge, Richard
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Martin, Adam
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Lee, Michael
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
December 1, 2007
Publication Information
Publication: NASA Tech Briefs, December 2007
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MFS-32364-1
Report Number: MFS-32364-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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