Characterization of Liquid Propellant for Improved LOTV Mission
Measurements of Laser Intensity Dependence of High Specific Impulse for Laser Ablative Propulsion
Spot Size Limited Carbon Propellant Characterization for Efficient High I~s~p Laser Propulsion
Impulse Generation Mechanism in Glycerin Propellant Laser Thruster
Fundamental Experiments on Glycerin Propellant Laser Thruster