Regression rate behaviors of HTPB-based propellant combinations for hybrid rocket motor
Effect of grain port length–diameter ratio on combustion performance in hybrid rocket motors
Effect of grain port length-diameter ratio on combustion performance in hybrid rocket motors
Optimal design of hybrid rocket motor powered vehicle for suborbital flight
Design and performance characterization of a sub-Newton N2O monopropellant thruster
Numerical simulation of the infrared radiative signatures of liquid and solid rocket plumes