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Werkstoff
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keywords:(Werkstoff)
A PREDICTIVE THERMO-ORBITAL MODEL FOR ANALYSIS OF SUN SYNCHRONOUS ORBITS OF NANOSATELLITES
DEVELOPMENT OF A THERMAL DESIGN MODEL FOR A SMALL SPACECRAFT WITH INTEGRATED HEAT PIPES
AEROTHERMAL ANALYSIS AND THERMAL PROTECTION OF GRID FINS FOR REENTRY ROCKETS
WHEN GSE BECOMES EQUALLY DEMANDING AS THE LIGHT WEIGHT STRUCTURE: A SOFT COVER FOR THE EUCLID BAFFLE
WHEEL DESIGN AND EXPERIMENTAL RESEARCH OF MANNED LUNAR ROVER
SOLAR SAIL ATTITUDE CONTROL USING AN INTEGRA TED SHAPE MEMORY ALLOY ACTUATOR
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
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
CUBESAT MAGNETIC ATLAS AND IN-ORBIT COMPENSATION OF RESIDUAL MAGNETIC DIPOLE
TARDIGRADE MECH: BORON NITRIDE NANOTUBE COMPOSITES FOR SPACE RADIATION PROTECTION
INVESTIGATIONS ON LIFEPO4/MWCNTS CATHODE FOR FLEXIBLE LI-ION BATTERIES
NANOMATERIALS IN SPACE: TECHNOLOGY INNOVATION & ECONOMIC TRENDS
DEVELOPMENT OF UVA STERILIZATION TECHNOLOGIES THAT CAN BE USED IN SPACE PLANT FACTORIES
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