KOSEN 한인과학기술자네트워크

[ Full-Length Papers ] - Shuttle Orviter Experimental Boundary-Layer Transition Results with Isolated Roughness - Trajectory-Based Thermal Protection Sizing for an X-33 Winged Vehicle Concept - Hybrid Euler/Particle Approach for Continuum/Rarefied Flows - Improved Satellite Drag Coefficient Calculations from Orbital Measurements of Energy Accommodation - Potential Flow Solutions with Wakes over an Ogive Cylinder - Aerodynamic Performance of Supersonic Missile Body-and Wing Tip-Mounted Lateral Jets - Fin Damage and Mass Offset for Kinetic Energy Projectile Spin/Pitch Lock-In - Experimental Inveestigation of Super-and Hypersonic Jet Interaction on Missile Configurations - Hinge Moment Coefficient Prediction for Nose-Mounted Canard Controls at Supersonic Speeds - Optimal External Configuration Design of Unguided Missiles - Trajectory Optimization Using Eccentric Longitude Formulation - Low-Thrust Eccentricity-Constrained Orbit Raising - Precision Orbit Determination for the Geosat Follow-On Satellites - Entry Guidance for the X-33 Vehicle - Mars Free Return Trajectories - Numerical Approach for Computing Noise-Induced Vibration from Launch Environments - Optimality of the Heating-Rate Constrained Aerocruise Maneuver - Launch Vehicles Self-Sustained Oscillation from Aeroelastic Coupling Part 1: Theory - Launch Vehicles Self-Sustained Oscillation from Aeroelastic Coupling Part 2: Analysis - Stiffness Design of Deployable Satellite Antennas in Deployed Configuration - Space Shuttle Main Engine Health Monitoring with Exhaust Plume Emission Spectroscopy