The purpose of this study is to establish the technical ground for modeling the physics of laser powered pulse detonation phenomenon. The principle of the laser power propulsion is that when high-powered laser is focused at a small area near the surface of a thruster, the intense energy causes the electrical breakdown of the working fluid (e.g. air) and forming high speed plasma (known as the inverse Bremsstrahlung, IB, effect). The intense heat and high pressure created in the plasma consequently causes the surrounding to heat up and expand until the thrust producing shock waves are formed. This complex process of gas ionization, increase in radiation absorption and the forming of plasma and shock waves will be investigated in the development of the present numerical model. In the first phase of this study, laser light focusing, radiation absorption and shock wave propagation over the entire pulsed cycle are modeled. The model geometry and test conditions of known benchmark experiments such as those in Myrabo's experiment will be employed in the numerical model validation simulations. The calculated performance data will be compared to the test data.Chen, Yen-Sen and Liu, Jiwen and Wei, HongMarshall Space Flight CenterLASER OUTPUTS; PULSED LASERS; PULSED RADIATION; PULSE DURATION; LASER PROPULSION; COMPUTATIONAL FLUID DYNAMICS; RADIATIVE HEAT TRANSFER; GAS IONIZATION; MATHEMATICAL MODELS; PLASMA WAVES; DETONATION WAVES; RADIATION ABSORPTION; SHOCK WAVE PROPAGATION; NONEQUILIBRIUM RADIATION; PLASMA RADIATION; WORKING FLUIDS; PRESSURE DISTRIBUTION; TEMPERATURE DISTRIBUTION; ELECTRON DENSITY PROFILES...