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
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
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
Werkstoffe im Automobilbau : ATZ, MTZ extra
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