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Single and Multi-Pulse Low-Energy Conical Theta Pinch Inductive Pulsed Plasma Thruster PerformanceFabricated and tested CTP IPPTs at cone angles of 20deg, 38deg, and 60deg, and performed direct single-pulse impulse bit measurements with continuous gas flow. Single pulse performance highest for 38deg angle with impulse bit of approx.1 mN-s for both argon and xenon. Estimated efficiencies low, but not unexpectedly so based on historical data trends and the direction of the force vector in the CTP. Capacitor charging system assembled to provide rapid recharging of capacitor bank, permitting repetition-rate operation. IPPT operated at repetition-rate of 5 Hz, at maximum average power of 2.5 kW, representing to our knowledge the highest average power for a repetitively-pulsed thruster. Average thrust in repetition-rate mode (at 5 kV, 75 sccm argon) was greater than simply multiplying the single-pulse impulse bit and the repetition rate.
Document ID
20130014226
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Hallock, Ashley K.
(Yetispace, Inc. Huntsville, AL, United States)
Martin, Adam
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Polzin, Kurt
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Kimberlin, Adam
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Eskridge, Richard
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 27, 2013
Publication Date
April 29, 2013
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M13-2607
Meeting Information
Meeting: 60th JNNAF Joint Propulsion Subcommittee Meeting
Location: Colorado Springs, CO
Country: United States
Start Date: April 29, 2013
End Date: May 3, 2013
Distribution Limits
Public
Copyright
Public Use Permitted.
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