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
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
APPLICATION OF MAGNETOCALORIC COOLING COMPONENTS FOR SMALL SATELLITE SYSTEMS
ADDITIVE MANUFACTURING OF SPATIALLY EFFICIENT, ARCHITECTURED MMOD SHIELDING
HEXAFLY-INT HYPERSONIC VEHICLE THERMAL PROTECTION SYSTEM DESIGN
ADDITIVE LAYER MANUFACTURING OF POLYMERIC NANOSAT!: AN HOLISTIC APPROACH
ON-ORBIT INSTALLATION MISSION PLANNING OF SPACE TRUSS WITH SQUARE CROSS-SECTION CONFIGURATION
DESIGN AND RESEARCH OF THERMAL PROTECTION CONSIDERING THE CARBON FROM MORPHOLOGY
DEVELOPMENT OF A DEGRADATION MODEL OF EPOXY ADHESIVE DUE TO RADIATION IN SPACE ENVIRONMENT
DYNAMIC ANALYSIS OF A NOVEL HEXAPOD PLATFORM WITH EMBEDDED ELECTROMAGNETIC SHUNT DAMPERS
PROTECTIVE HEAT RESISTANT COATING FOR INCONEL 718 ADDITIVELY MANUFACTURED PARTS
FRACTURE CONTROL FOR ADDITIVELY MANUFACTURED SPACECRAFT STRUCTURES
PW-SAT2 DEORBIT SAIL TEST CAMPAIGN AT DROP TOWER AND VERIFICATION ON ORBIT
DIAGNOSTICS OF DEFECTS OF THERMAL PROTECTIONS INFLATABLE RE-ENTRY VEHICLES
INVESTIGATION OF THE IMPACT CONDITIONS OF A MECHANICAL SHOCK TEST FACILITY
DEVELOPMENT OF LARGE HIGH PRESSURIZED XENON TANK FOR ELECTRICAL PROPULSION SYSTEMS
COOLING CHANNEL AT THE LEADING EDGE OF SUPERSONIC VEHICLE DESIGN BASED ON WORKING FLUID CONVECTION
EFFECTS OF LONG-TERM EXPOSURE TO THE LOW-EARTH ORBIT ENVIRONMENT ON DRAG AUGMENTATION SYSTEMS
STABILITY THEORY METHODOLOGY IN PROBLEM.OF THE MOTIONS SEPARATION FOR SGS