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Werkstoff
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INVESTIGATION OF THE IMPACT CONDITIONS OF A MECHANICAL SHOCK TEST FACILITY
DEVELOPMENT OF LARGE HIGH PRESSURIZED XENON TANK FOR ELECTRICAL PROPULSION SYSTEMS
TOPOLOGY OPTIMIZATION FOR 3D PRINTING WITH SELECTIVE PLACEMENT OF CNT YARN REINFORCEMENT
SENSOR COATINGS FOR HIGH-TEMPERATURE MEASUREMENTS IN SPACE APPLICATION
SUITABILITY OF MANUFACTURING PROCESSES FOR IN-SPACE MANUFACTURING OF SPACECRAFT COMPONENTS
THE PERMIAM™ ADDITIVE MANUFACTURING PROCESS FOR OPEN POROSITY IN
AN OVERVIEW OF THE APPLICATION OF 3D PRINTED SPACECRAFT STRUCTURES WITHIN THE REDSHIFT PROJECT
SLS PRODUCTION FRICTION STIR PLUGS BY SOLID STATE ADDITIVE DEPOSITION
EXPERIMENTAL VERIFICATION OF TWO-DIMENSIONAL SELF-DEPLOYABLE SPACE STRUCTURES WITH CONVEX-PANEL
A NEW DEVICE AND METHOD FOR SIMULATING HYPERSONIC AEROTHERMAL ENVIRONMENT
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
ANISOTROPIC HEAT-SHIELDING MATERIALS: PROSPECTS FOR APLICATION IN THE RE-ENTRY MODULE HEAT SHIELD
DIAGNOSTICS OF DEFECTS OF THERMAL PROTECTIONS INFLATABLE RE-ENTRY VEHICLES
STRUCTURAL DESIGN AND ANALYSIS OF AN AEROSHELL FOR A HUMAN CREW ENTRY VEHICLE IN MARTIAN ATMOSPHERE
ENGINEERING CHALLENGES IN CONFIGURING A MODULAR CRYOGENIC UPPER STAGE
MOTION ESTIMATION OF MEMBRANE SPACE STRUCTURE USING ORBIT MEASUREMENT DATA
STATIC AND DYNAMIC CHARACTERIZATION OF A METALLIC COMPONENT OF VEGA-C INTERSTAGE 2/3
THERMAL ANALYSIS AND TVAC TESTING OF THE HOPE PROBE (EMIRATES MARS MISSION)
A NEW MODELING METHOD BASED ON MODAL VARIABLES FOR POGO ANALYSIS OF LIQUID ROCKETS
VIBRATION ANALYSIS OF PIEZOELASTIC SPACE-STRUCTURE FOR ENERGY HARVESTER
SHADOW THERMAL CYCLING AND ITS EFFECT ON SOLAR ARRAY PREDICTED EOL TIME
Innovative manufacturing of 3D-Textile-Sheet Metal-Composites
CUBESAT THERMAL ANALYSIS AND DESIGN: TECHNIQUES AND REFERENCE GUIDELINES FOR CUBESAT DEVELOPERS
STUDIES ON LUNAR LANDER STABILITY BEHAVIOUR USING A 1/6TH SCALE MODEL
FEASIBILITY AND SPONTANEITY OF GEOPOLYMERS FOR POTENTIAL AEROSPACE APPLICATIONS