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Leonard D. Cassady, Ph.D. - Publications

Affiliations: 
2006 Princeton University, Princeton, NJ 
Area:
Fluid and Plasma Physics, Aerospace Engineering
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16 high-probability publications. We are testing a new system for linking publications to authors. You can help! If you notice any inaccuracies, please sign in and mark papers as correct or incorrect matches. If you identify any major omissions or other inaccuracies in the publication list, please let us know.

Year Citation  Score
2014 Longmier BW, Squire JP, Olsen CS, Cassady LD, Ballenger MG, Carter MD, Ilin AV, Glover TW, McCaskill GE, Díaz FRC, Bering EA. Improved efficiency and throttling range of the VX-200 magnetoplasma thruster Journal of Propulsion and Power. 30: 123-132. DOI: 10.2514/1.B34801  0.46
2014 Sheehan JP, Longmier BW, Bering EA, Olsen CS, Squire JP, Ballenger MG, Carter MD, Cassady LD, Chang Díaz FR, Glover TW, Ilin AV. Temperature gradients due to adiabatic plasma expansion in a magnetic nozzle Plasma Sources Science and Technology. 23. DOI: 10.1088/0963-0252/23/4/045014  0.404
2012 Longmier BW, Squire JP, Olsen CS, Cassady LD, Ballenger MG, Carter MD, Ilin AV, Glover TW, McCaskill GE, Chang Díaz FR, Bering EA. VASIMR® VX-200 improved throttling range 48th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2012.  0.452
2011 Longmier BW, Cassady LD, Ballenger MG, Carter MD, Chang-Díaz FR, Glover TW, Ilin AV, McCaskill GE, Olsen CS, Squire JP, Bering EA. VX-200 magnetoplasma thruster performance results exceeding fifty-percent thruster efficiency Journal of Propulsion and Power. 27: 915-920. DOI: 10.2514/1.B34085  0.481
2011 Longmier BW, Bering EA, Carter MD, Cassady LD, Chancery WJ, Díaz FRC, Glover TW, Hershkowitz N, Ilin AV, McCaskill GE, Olsen CS, Squire JP. Ambipolar ion acceleration in an expanding magnetic nozzle Plasma Sources Science and Technology. 20. DOI: 10.1088/0963-0252/20/1/015007  0.411
2011 Bering EA, Longmier BW, Olsen CS, Cassady LD, Squire JP, Chang Díaz FR. VASIMR®: Deep space transportation for the 21st century Aiaa Space Conference and Exposition 2011.  0.479
2009 Mulcahy JM, Browne DJ, Stanton KT, Chang Diaz FR, Cassady LD, Berisford DF, Bengtson RD. 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. DOI: 10.1016/J.Ijheatmasstransfer.2008.10.031  0.369
2009 Longmier BW, Squire JP, Carter MD, Cassady LD, Glover TW, Chancery WJ, Olsen CS, Ilin AV, McCaskill GE, Díaz FRC, Bering EA. Ambipolar ion acceleration in the expanding magnetic nozzle of the VASIMR® VX-200i 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit.  0.316
2009 Cassady LD, Chancery WJ, Longmier BW, Olsen C, McCaskill G, Carter M, Glover TW, Squire JP, Diaz FRC, Bering EA. VASIMR® technological advances and first stage performance results 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit.  0.442
2008 Berisford DF, Bengtson RD, Raja LL, Cassady LD, Chancery WJ. Heat flow diagnostics for helicon plasmas. The Review of Scientific Instruments. 79: 10F515. PMID 19044660 DOI: 10.1063/1.2955710  0.447
2008 Bering EA, Chang-Díaz FR, Squire JP, Brukardt M, Glover TW, Bengtson RD, Jacobson VT, McCaskill GE, Cassady L. Electromagnetic ion cyclotron resonance heating in the VASIMR Advances in Space Research. 42: 192-205. DOI: 10.1016/J.Asr.2007.09.034  0.316
2007 Bering EA, Chang-Díaz FR, Squire JP, Jacobson V, Cassady LD, Brukardt M. High power ion cyclotron heating in the VASIMR engine Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 10: 7068-7081.  0.407
2007 Bering EA, Glover TW, Chang-Díaz FR, Squire JP, Cassady LD, Brukardt M. VASIMR™: A private enterprise solution to space transportation beyond LEO A Collection of Technical Papers - Aiaa Space 2007 Conference. 2: 1523-1542.  0.417
2004 Sankaran K, Cassady L, Kodys AD, Choueiri EY. A survey of propulsion options for cargo and piloted missions to Mars. Annals of the New York Academy of Sciences. 1017: 450-67. PMID 15220162 DOI: 10.1196/Annals.1311.027  0.472
2003 Kodys AD, Cassady LD, Choueiri EY. Thermal effects on inverted pendulum thrust stands for steady-state high-power plasma thrusters 39th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit.  0.503
2002 Cassady LD, Kodys AD, Choueiri EY. A thrust stand for high-power steady-state plasma thrusters 38th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit.  0.552
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