TOTAL IONIZING DOSE (TID) TESTING OF DC-DC CONVERTERS IRRADIATED WITH CO-60 SOURCE
INNOVATIVE 3D PRINTED SOFT MAGNETS FOR SATELLITE ELECTRIC MOTORS
ANALYZING QUASI-STATIC AND DYNAMIC RESPONSES OF A 3U CUBESAT STRUCTURE DURING LAUNCHING
REMOTE-SENSING SATELLITE:THE DEVELOPMENT OF COUPLE RING TYPE THERMO-REFOCUSING MECHANISM
MODELING AND ANALYSIS OF CONTACT-IMPACT DYNAMICS OF A SPACE FLEXIBLE NET WITH AN INFLATABLE BOOM
LOW COST FILAMENT-WINDING TECHNOLOGY FOR SMALL AEROSPACE LABORATORIES AND STARTUPS
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
THERMO-MECHANICAL DESIGN AND ANALYSIS OF A MULTISPECTRAL IMAGING PAYLOAD USING PHASE CHANGE MATERIAL
FLEXIBLE AND SCALABLE THERMAL DESIGN OF MODULAR ON-ORBIT ASSEMBLY MICROSATELLITE
FEASIBILITY STUDY ON ADDITIVE MANUFACTURING OF CUBESAT STRUCTURES
RESEARCH OF SATELLITE SEPARATION ATTITUDE BASED ON MONTE CARLO METHOD
THE RADIATION ENVIRONMENT AND EFFECTS ANALYSIS OF THE LUMIO MISSION
DYNAMIC RESPONSE AND BEHAVIOR SIMULATION OF A THERMAL BOOT EMPLOYED IN A HEAVY LIFT LAUNCH VEHICLE
LTO-MWCNTS BASED NANOCOMPOSITE FLEXIBLE ELECTRODES FOR LI ION BATTERIES
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
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
ERROR DISTRIBUTIONS IN A HIGH-PRECISION DOCKING SYSTEM DESIGN OF MICRO-SATELLITES
CONTROL-ORIENTED MODELLING OF AN ACTIVE SUPPRESSION SYSTEM FOR LARGE SPACE SMART STRUCTURES