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Michael W. Martin, PhD.
Michael W. Martin, PhD.
Benchmark Space Systems
Verified email at benchmark-space.com
Title
Cited by
Cited by
Year
Determination of regression rate in an ablating hybrid rocket solid fuel using a physics based comprehensive mathematical model
K Akyuzlu, A Antoniou, M Martin
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 3577, 2002
202002
Volumetric efficiency and pumping torque estimation and compressor recirculation control of turbocharged engines
M Martin
SAE World Congress e Exhibition,(SAE 2009-01-0587), 2009
52009
Method to Simulate Spacecraft Electrical Surface Charging due to Magnetoplasma Engine Plume-Spacecraft Interaction
MW Martin, D Staack, T Lalk
2018 Joint Propulsion Conference, 4507, 2018
2018
Method to Simulate Magnetoplasma Engine Plume-Spacecraft Interaction
MW Martin, T Lalk, D Staack
53rd AIAA/SAE/ASEE Joint Propulsion Conference, 4722, 2017
2017
Prediction of Damage to Structure resulting from Recirculation of Particles from a Magnetoplasma Spacecraft Engine
MW Martin
2014
Ecclesia semper reformanda: Welche Impulse für die Kirche und ihre Reform erwartet die ELKB?
MW Martin
Luthers Unvollendete, 69-80, 2013
2013
Simulation of Particle Recirculation in the VASIMR® Plasma Engine Backfield
M Martin, T Lalk, D Staack
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 3931, 2012
2012
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