Leonard D. Cassady, Ph.D.

Affiliations: 
2006 Princeton University, Princeton, NJ 
Area:
Fluid and Plasma Physics, Aerospace Engineering
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"Leonard Cassady"

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Edgar Y. Choueiri grad student 2001-2006 Princeton
 (PhD Thesis: Lithium -fed arc multichannel and single-channel hollow cathode: Experiment and theory.)
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Publications

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Longmier BW, Squire JP, Olsen CS, et al. (2014) Improved efficiency and throttling range of the VX-200 magnetoplasma thruster Journal of Propulsion and Power. 30: 123-132
Sheehan JP, Longmier BW, Bering EA, et al. (2014) Temperature gradients due to adiabatic plasma expansion in a magnetic nozzle Plasma Sources Science and Technology. 23
Longmier BW, Squire JP, Olsen CS, et al. (2012) VASIMR® VX-200 improved throttling range 48th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2012
Longmier BW, Cassady LD, Ballenger MG, et al. (2011) VX-200 magnetoplasma thruster performance results exceeding fifty-percent thruster efficiency Journal of Propulsion and Power. 27: 915-920
Longmier BW, Bering EA, Carter MD, et al. (2011) Ambipolar ion acceleration in an expanding magnetic nozzle Plasma Sources Science and Technology. 20
Bering EA, Longmier BW, Olsen CS, et al. (2011) VASIMR®: Deep space transportation for the 21st century Aiaa Space Conference and Exposition 2011
Mulcahy JM, Browne DJ, Stanton KT, et al. (2009) Heat flux estimation of a plasma rocket helicon source by solution of the inverse heat conduction problem International Journal of Heat and Mass Transfer. 52: 2343-2357
Longmier BW, Squire JP, Carter MD, et al. (2009) Ambipolar ion acceleration in the expanding magnetic nozzle of the VASIMR® VX-200i 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit
Cassady LD, Chancery WJ, Longmier BW, et al. (2009) VASIMR® technological advances and first stage performance results 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit
Berisford DF, Bengtson RD, Raja LL, et al. (2008) Heat flow diagnostics for helicon plasmas. The Review of Scientific Instruments. 79: 10F515
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