ARCHITECTED CERAMIC STRUCTURES FOR HIGH TEMPERATURE APPLICATIONS
FINITE ELEMENT ANALYSIS AND VIBRATION TESTING OF THE MYSAT-2 CUBESAT
SHAPE CONTROL OF SOLAR SAIL USING SELECTIVE OPERATION OF MEMBRANE MOUNTING SMA WIRES
CUBESAT THERMAL ANALYSIS AND DESIGN: TECHNIQUES AND REFERENCE GUIDELINES FOR CUBESAT DEVELOPERS
STUDIES ON LUNAR LANDER STABILITY BEHAVIOUR USING A 1/6TH SCALE MODEL
STUDY AND DEVELOPMENT OF SATELLITE SOLAR PANELS DEPLOYMENT SYSTEM
SPACE-GRADE POLYETHYLENE/CARBON NANOCOMPOSITES FABRICATED BY 3D- PRINTING
ANALYSIS OF INFLUENCES OF EXTERNAL COMPONENTS DURING VIBRATION TESTING OF CIBESATS
MECHANICAL PROPERTIES OF POLYMER-DERIVED CERAMICS MODIFIED BY ACTIVE AND PASSIVE NANO-PARTICLES
ENVIRONMENTAL ANALYSIS OF NANOROVERS IN A SWARM FOR LUNAR'S SCIENTIFIC MISSIONS
THERMAL DESIGN STRATEGY UTILIZING TRANSFORMABLE STRUCTURE OF SPACECRAFT
NEW APPROACH TO SEMI-ACTIVE VIBRATION CONTROL BASED ON DISTURBANCE PREDICTION
ELECTRODYNAMIC DUST SHIELD TESTING ON THE MATERIALS ON INTERNATIONAL SPACE STATION EXPERIMENT
KEYNOTE: DISCOVERER - MAKING COMMERCIAL SATELLITE OPERATIONS IN VERY LOW EARTH ORBITS A REALITY
LABORATORY DEMONSTRATION OF COHERENT COMBINATION OF SPARSE APERTURE IMAGES
ESTIMATION OF DYNAMIC STRESSES IN CONNECTING LEADS OF SMC ON PCB FOR LAUNCH LOADS
CFD ANALYSIS OF ACOUSTIC DAMPING ON HELMHOLTZ RESONATORS INSIDE ROCKETS COMBUSTION CHAMBERS
INFLUENCE OF CARBON NANOTUBE ACTUATOR BY SPACE ENVIRONMENTAL FACTORS
AERODYNAMIC HEATING REDUCTION WITH JET ARRAYS OVER THE SHARP EDGE OF A HYPERSONIC VEHICLE
THERMAL CONTROL DESIGN OF HIGH-POWER SMALL SATELLITE ORBITING MARS
FEASIBILITY AND SPONTANEITY OF GEOPOLYMERS FOR POTENTIAL AEROSPACE APPLICATIONS
VIBRATION TEST FOR 7 TON-CLASS LIQUID PROPELLANT ROCKET ENGINE
OPTIMIZING TOPOLOGY AND STACKING SEQUENCE IN LAMINATED COMPOSITE STRUCTURES
DYNAMIC STALL CHARACTERISTICS OF LOW REYNOLDS NUMBER AIRFOIL IN MARTIAN AND TITAN'S ATMOSPHERE
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF PIEZOELECTRIC ENERGY HARVESTER BASED ON FLAG-FLUTTER
NONLINEAR SYSTEM IDENTIFICATION OF EXTENSIBLE TRUSS WITH MECHANICAL BACKLASHES
MICROVIBRATION ENGINEERING - A KEY TO HIGH-PERFORMANCE SPACE MISSIONS
THERMAL ANALYSIS AND TVAC TESTING OF THE HOPE PROBE (EMIRATES MARS MISSION)