63rd International Astronautical Congress 2012

(IAC 2012)

Naples, Italy 1-5 October 2012

Volume 8 of 14

ISBN: 978-1-62276-979-7 ISSN: 1995-6258 VOLUME 8

CIRCUMLUNAR FREE RETURN TRAJECTORY IAC-I2.C1.7.13 HIGH-ACCURACY ASYMMETRIC 5940 DESIGN WITH HIGH-LATITUDE LANDING FOR CHINA Slung Yik Yim

C1.8. ATTITUDE DYNAMICS (1)

A COMPRISED OF IAC-I2.C1.8.1 COUPLED ORBIT AND ATTITUDE DYNAMICS FOR SPACECRAFT 5951 MULTIPLE BODIES IN EARTH-MOON HALO ORBITS Amanda Knutson 5966 IAC-I2.CI.8.2 AOCS SCIENCE MODE DESIGN FOR ESAHS EUCLID MISSION Alberto Anselnu OF SPACE STATION IAC-12.C1.8.3 ZERO-PROPELLANT ATTITUDE MANEUVER PATH PLANNING 5968 BASED ON SIMPLE GIMBAL CONTROL MOMENT GYROSCOPES Huj-flinji Huang FOR SPINNING IAC-12.C1.8.4 ROBUSTNESS ANALYSES OF ATTITUDE SLEW MANOEUVRES 5974 PENETRATOR SPACECRAFT Robin Rous SUPPORT IAC-12.CI.8.5 REX-J (ROBOT EXPERIMENT ON ISS/JEM) TO DEMONSTRATE ASTRONAUT 5991 ROBOT - RESULT OF THE IN-ORBIT CHECK OUT OF THE REX-J MISSION Mit\ushtge (kia IAC-12.C1.8.6 DEVELOPMENT OF SUN-POINTING MAGNETIC ATTITUDE CONTROL SYSTEM FOR CXBN CUBESAT 5992 I'aruie Teslani IAC-I2.C1.8.7 DYNAMIC MODELLING AND CONTROL OF FLEXIBLE ROBOTIC SPACE MANIPULATORS WITH TELESCOPING BOOMS 5998 Alex HWi/i IAC-12.C1.8.8 FIRST IN-ORBIT RESULTS OF THE PLEIADES CMC-BASED ATTITUDE CONTROL SYSTEM 6009 ('htirles Koeck 1AC-12.C1.8.9 SPACE MANIPULATOR CONTROL FOR THE DYMAFLEX FLIGHT EXPERIMENT 6020 Xicholas P'Amore IAC-12.C1.8.10 INVESTIGATION OF ON-ORBIT ELECTODYNAMIC TETHER DEPLOYMENT BY GROUND EXPERIMENT AND NUMERICAL SIMULATION USING A DETAILED FRICTION MODEL 6029 .\tilsuhisa Riibii

1 VC-12.C1.8.U EXPERIMENTAL ORBITAL RENDEZVOUS OPERATIONS VIA VISUAL BASED TECHNIQUES 6038 Mann S*ihtttni

1AC-12.CI.8.12 PATH PLANNING OF EXPERIMENTAL MODULE TRANSFER FOR MINIMIZING ATTITUDE DISTURBANCE OF SPACE STATION 6052 i t H ang IAC-12.C1.8.13 A SENSITIVITY ANALYSIS APPROACH IN THE DESIGN OF THE ATTITUDE CONTROL OF SMALL SATELLITES SYSTEM 6058 Marius Sloia-Djeska

C1.9. ATTITUDE DYNAMICS (2)

NEURAL-NETWORK-BASED IAC-12.C1.9.1 WIDE-FOV CMOS SUN SENSOR 6070 Michele Grassi IAC-12.C1.9.2 PRACTICAL APPROACH FOR QUICK ATTITUDE MANEUVER OF SPACECRAFT WITH ACTUATOR SATURATION 6080 Hyosang Yoon IAC-12.C1.9.3 SDS-4 ATTITUDE CONTROL SYSTEM: FIRST FLIGHT RESULTS OF ATTITUDE CONTROL RESPONSE 6087 Yuta Nakajima IAC-12.C1.9.4 DYNAMICS OFA TETHER CONNECTED TO AN IRREGULAR SHAPED CELESTIAL BODY 6094 MohammadJ. Mashayekhi IAC-12.C1.9.5 RACS QFR ALGORITHM FOR VEGA FPSA PROGRAM 6101 Giovanni Cuciniello

IAC-12.C1.9.6 DUAL ATTITUDE AND PARAMETER ESTIMATION OF PASSIVELY MAGNETICALLY STABILIZED SPACECRAFT 6111 Roland Burton

IAC-12.C1.9.7 ATTITUDE MOTION PLANNING FOR A SPIN STABILISED DISK SAIL 6122 Craig Maclean IAC-12.C1.9.8 CONTROLLABILITY OF PROPELLANT-FREE ATTITUDE CONTROL SYSTEM FOR SPINNING SOLAR SAIL USING THIN-FILM REFLECTIVITY CONTROL DEVICES CONSIDERING ARBITRARY SAIL DEFORMATION 6131 Ryu Funase IAC-I2.C1.9.9 COUPLED ORBITAL AND ATTITUDE CONTROL OF SPACECRAFT IN FORMATION 6139 Mania Zamaro

IAC-12.C1.9.10 COUPLED ORBIT AND ATTITUDE DYNAMICS OF A RECONFIGURABLE SPACECRAFT WITH SOLAR RADIATION PRESSURE 6140 Andreas Borggrafe IAC-12.C1.9.11 ATTITUDE DETERMINATION OF ABOUT ONE DEGREE ACCURACY USING ONLY MAGNETOMETER DATA IN MEGHA-TROPIQUES 6150 Ritu Karidhal

IAC-12.C1.9.12 DEVELOPMENT, COMPLEX INVESTIGATION, LABORATORY AND FLIGHT TESTING OF THE MAGNETO-GYROSCOPIC ACS FOR THE MICROSATELLITE 6157 Michael Yu. Ovchinnikov

IAC-12.C1.9.13 OPTIMAL ATTITUDE MANEUVER PATH PLANNING FOR SPACECRAFT UNDER COMPLEX GEOMETRY CONSTRAINTS 6172 Qian Zhao

C2. MATERIALS AND STRUCTURES SYMPOSIUM

C2.1. - SPACE STRUCTURES 1 DEVELOPMENT AND VERIFICATION (SPACE VEHICLES AND COMPONENTS)

IAC-12.C2.1.1 SIMULATION OF VEGA DYNAMIC ENVIRONMENT BY USING PROPELLANT COMPLEX CHARACTERIZATION 6178 C. Di Trapani IAC-12.C2.1.2 DESIGN OF A COPV FOR LIQUID STORABLE PROPELLANTS OF 4 STAGE VEGA LAUNCHER 6186 A. Mataloni IAC-12.C2.1.3 PRACTICAL APPLICATION OF DIC IN FATIGUE AND FRACTURE TOUGHNESS TESTING 6195 Fawad Tariq IAC-12.C2.1.4 A RESEARCH ON SHOCK PREDICTION METHOD CORRELATED WITH FORMOSAT-2 SATELLITE PYRO-SHOCK TEST RESULTS 6208 Chi-Wei Chou

IAC-12.C2.1.5 DEVELOPMENT OF A STRUCTURAL MODEL FOR KOREAN LUNAR EXPLORER 6215 Taek-Joon Son

IAC-12.C2.1.6 STANDARD FEM VALIDATION CHECKS AND QUALITY OF RESPONSE PREDICTION 6216 Guglielmo Agliet IAC-12.C2.I.7 ANALYSIS OF PROCESS-INDUCED DEFORMATION OF COMPLICATED COMPOSITE CURVED SURFACE 6223 Yizhi Fu THE AND NEW METHODOLOGY FOR MEASURING IAC-12 C2 1 8 NOVEL TECHNOLOGIES FROM MATERIALS AND OF (SEMI) VOLATILE ORGANIC COMPOUNDS CONTAMINATION 6224 ENVIRONMENTS. ( aniline Wlddowsan HEATSHIELD AND POST-FLIGHT ANALYSIS OF THE RECOVERED HAYABUSA 1AC-12.C2.1.9 6227 RESULTS FROM AIRBORNE OBSERVATION Tetsuya Yamada FOR WIND TUNNEL TESTING AND IAC-I2.C2.1.I0 INSTRUMENTATION OF THE EXPERT FLAP 6237 EVALUATION OF TEST RESULTS Thomas Thiele EMISSIVITY OF THE EXPERT FLAP IN IAC-12.C2.1.11 EXPERIMENTAL INVESTIGATION OF THE 6248 SCTROCCO PLASMA WIND TUNNEL TESTS ('aria Purpura BOOSTER FLEX NOZZLE IAC-12.C2.1.12 DESIGN CONSIDERATIONS FOR SOLID ROCKET 6254 HARDWARE Atha ilr Rahman Khan 6261 IAC- I2.C2.1.13 LARES SYSTEM DEVELOPMENT AND VERIFICATION Alejandro Hurst HIGH SPEED VEHICLES IAC-12.C2.1.14 PREDICTION OF TRANSIENT SKIN TEMPERATURE OF 6271 THROUGH CFD Muhammad-Nauman Oureshi MANIPULATOR SYSTEM IAC-12.C2.1.15 NONLINEAR FEEDBACKCOMPOSITE CONTROL OF SPACE 6272 WITH BOUNDED TORQUE INPUTS AND UNCERTAIN PARAMETERS die Liang CERAMIC IAC-12.C2.1.16 THERMO-STRUCTURAL DESIGN OF ULTRA HIGH TEMPERATURE (UHTC) 6279 WINGLETS OF A RE-ENTRY SPACE VEHICLE Hoherto Saghano LARES IAC-12.C2.1.17 QUALIFICATION TESTS ON THE OPTICAL RETRO-REFLECTORS OF 6280 SATELLITE. Antonio Paolozzi WEIGHT IAC-12.C2.1.18 OPTIMIZATION OF MARTIAN REGOLITH AND ULTRA-HIGH MOLECULAR POLYETHYLENE COMPOSITES FOR RADIATION SHIELDING AND HABITAT STRUCTURES 6287

Milan Barnett

C2.2. SPACE STRUCTURES 2 - DEVELOPMENT AND VERIFICATION (DEPLOYABLE AND DIMENSIONALLY STABLE STRUCTURES

IAC-12.C2.2.1 PRESSURIZED STRUCTURES FOR SUPPORTINGTHE HUMAN PRESENCE IN SPACE. HIGHLIGHT OF THE ITALIAN CONTRIBUTION 6288 Ernesto Valleram IAC-12.C2.2.2 OPTIMIZATION METHOD ON CONTROLLING THERMAL DEFORMATION OF LARGE SPACE DEPLOYABLE TRUSS STRUCTURES 6306 Shu/ie Zhang IAC-12.C2.2.3 OPERATIONAL MODAL ANALYSIS VIA IMAGE BASED TECHNIQUE OF VERY FLEXIBLE SPACE STRUCTURES 6311 Afurco Sahatmi IAC-I2.C2.2.4 STUDY ON A CALIBRATION METHOD FOR SHAPE CONTROL PARAMETERS OF A SELF- SENSING REFLECTOR ANTENNA EQUIPPED WITH SURFACE ADJUSTMENT MECHANISMS 6322 HinHiki Tanaka IAC-12.C2.2.5 THALES ALENIA SPACE FLIGHT HERITAGE IN DEPLOYMENT PREDICTION OF LARGE DEPLOYABLE STRUCTURES 6330 Anne ('arpme IAC-12.C2.2.6 STRUCTURAL AND DYNAMIC ANALYSIS OF A LONG SELF DEPLOYING ANTENNA FOR JUPITER GANYMEDE ORBITER SUB SURFACE SOUNDER 6336 Mirco Zuccartatta

IAC-12.C2.2.7 A SIMPLE DEPLOYMENT MECHANISM OF PANEL STRUCTURE FOR MICRO SATELLITE AND ITS VERIFICATION 6338 Yasu\vki Miyxizaki 1 A( -12.C2.2.8 CONTROL PARAMETERS TRANSITION DURING DEPLOYING OPERATIONS OF A SPACE FLEXIBLE STRUCTURE VIA MULTI-BODY APPROACH 6339 A/i/ru/ Safhitm

1.VC-12.C2.2.9 STEPWISE DEPLOYMENT OF MEMBRANE SPACE STRUCTURES - ROLLED-UP TOGETHER WITH SUPPORT BOOMS 6350 M (' Xaton

IAC-12.C2.2.10 EFFECT OF SHAPE IMBALANCE ON SPINNING MEMBRANE DEPLOYMENT FOR SOLAR SAIL OJ31

.. . kengv Sninlaku... IAC -12.C 2.2.11 DESIGN OF DEBRIS REMOVAL MISSIONS PERFORMED BY ROBOTIC GRASPERS 6356 (itovanm H f\ilmt-rtni BUCKLING DESIGN OF BOOM BY IAC-12.C2.2.12 STRUCTURES FEM ANALYSIS 6367 Susanna Laurenzi

C2.3. SPACE STRUCTURES - DYNAMICS AND MICRODYNAMICS

IAC-12.C2.3.1 VIBRATION ISOLATION PLATFORM OF CMGS APPLICATION ON SATELLITES WITH THE APPENDAGES FLEXIBLE 6372 Yao Zhang IAC-12.C2.3.2 ANALYSIS OF MICRO-VIBRATION BY HIGH RESOLUTION FORCE SENSING MEASUREMENT TO REDUCE MECHANICAL NOISE 6380 Florian Heboid IAC-12.C2.3.3 A GENERAL METHODOLOGY TO STUDY THE TRANSMISSION OF MICRO-VIBRATIONS IN SATELLITES 6386 Marcello Remedia

IAC-12.C2.3.4 ANALYSIS AND VERIFICATION OF MICRO-VIBRATIONS ON SATELLITE LEVEL 6394 Robert Engel IAC-12.C2.3.5 BE-FE ACOUSTIC-STRUCTURAL COUPLING ANALYSIS FOR DYNAMIC RESPONSE OF SPACECRAFT COMPOSITE SHELLS 6395 Hahjono Djojodihardjo IAC-12.C2.3.6 VERY LARGE SPACE STRUCTURES: NON-LINEAR CONTROL AND ROBUSTNESS TO STRUCTURAL UNCERTAINTIES 6415 Paolo Gasbarri

IAC-12.C2.3.7 THE IMPACT OF THE SLOSHING MOTION COMBINED WITH FLEXIBILITY OF SPACECRAFT COMPONENTS IN THE DESIGN OF ATTITUDE AND ORBIT CONTROL SUBSYSTEMS 6432 IjarM. Da Fonseca IAC-12.C2.3.8 BENEFITS AND CONSTRAINTS IN REPLACING LOW-EFFICIENCY WATER-COOLED LINEAR POWER AMPLIFIERS BY NEW AIR-COOLED CLASS-D AMPLIFIERS FOR DRIVING VIBRATION TESTING SYSTEMS 6444 Durval Zandonadi Jr. IAC-12.C2.3.9 CUMULATIVE MEASUREMENT ERRORS FOR DYNAMIC TESTING OF SPACE FLIGHT HARDWARE 6450 Susan Winnitoy IAC-12.C2.3.10 NEW OPTIMIZATION APPROACH FOR MULTIPLE DYNAMIC VIBRATION ABSORBERS 6451 Yohsuke Nambu

IAC-12.C2.3.11 DYNAMIC BEHAVIOR ANALYSIS OF INFLATABLE BOOMS IN ZIGZAG AND MODIFIED ZIGZAG FOLDING PATTERNS 6462 Nobuisa Kalsumata

IAC-12.C2.3.12 NUMERICAL VALIDATION OF RADOM ENERGY FLOW ANALYSIS FOR COUPLED BEAM STRUCTURES BASED FEA ON AND SEA APPROACHES 6474 Jin You IAC-12.C2.3.13 MECHANICAL ENVIRONMENT TESTS OF CHINA COMMUNICATION SATELLITE 6475 Zhengju Li IAC-12.C2.3.I4 ENERGY SENSITIVITY BASED METHOD FOR IDENTIFICATION OF STATISTICAL ENERGY ANALYSIS PARAMETERS 6476 Hongliang Zhang IAC-12.C2.3.I5 STUDY ON POGO VIBRATION SUPPRESSION OF GAS-LIQUID FLOW IN CRYOGENIC PUMP FEED LINE 6487 Jie Fang IAC-12.C2.3.16 IN-ORBIT MICRO-VIBRATION MEASUREMENT OF CASTHS ZY-3 SATELLITE 6488 Gaofeng Guo IAC-12.C2.3.17 ESTIMATION OF INERTIA PARAMETERS FOR ON-ORBIT OBJECT USING A ROBOT ARM 6489 Shuguang Li IAC-12.C2.3.I8 RESEARCH ON THE MODAL TEST TECHNOLOGY FOR THE LARGE LAUNCH VEHICLE WITH FOUR BOOSTERS 6490 PengHui Wang

IAC-12.C2.3.19 LANDING LOADS ANALYSIS OF LUNAR LANDER USING MONTE CARLO METHOD 6500 Dongping Liang

C2.4. NEW MATERIALS AND STRUCTURAL CONCEPTS

IAC-12.C2.4.I INNOVATIVE THERMAL PROTECTION SYSTEM FOR RE-ENTRY APPLICATION 6501 Maria Albano

IAC-12.C2.4.2 SHARP COMPOSITE UHTC LEADING EDGES FOR HYPERSONIC APPLICATIONS 6505 Frederic Monteverde IAC-12.C2.4.3 FIBER REINFORCED UHTC AND UHTC COATED METALS PAYLOADS ON THE AUSTRALIAN HYPERSONIC VEHICLE SCRAMSPACE 6512 Roberto Gardi THERMAL LIGHT-WEIGHT SI02-AL203 AEROGELS FOR HIGH-TEMPERATURE IAC-I2.C2.4.4 6513 INSULATION Junning Li FOR NEXT GENERATION SPACE CARBON NANOTUBES COMPOSITES: MATERIAL IAC-12.C 2.4.5 6514 VEHICLE Siihaib Akhur AS LIGHT-WEIGHT AND DURABLE STRUCTURAL 1AC-I2.C2.4.6 CARBON HONEYCOMB PLASTIC 6519 MATERIAL {'itloihmvr .STyvvmAv' METAL MATRIX COMPOSITES FOR USE IN AEROSPACE IAC-12.C2.A.7 FRICTION STIR WELDING OF 6530 STRUCTURES Tracie Prater IN PRESENCE OF VOIDS AND INCLUSIONS USING IAC-12.C2.4.8 CRACK PROPAGATION MODELLING 6539 A PERIDYNAMIC APPROACH Miru> Zaecanoto BY MEANS OF ELECTROACTIVE POLYMERS 6540 IAC-12.C2.4.9 NOVEL ROLLING ROVERS ACTUATED Stefano Zampienn ABSORPTION BY NANO PARTICLES 6541 IAC-12.C2.4.10 ENHANCEMENT OF OPTICAL Yongan Tang TECHNOLOGY ON FUTURE SPACE IAC-I2.C2.4.11 THE IMPACT OF STRUCTURAL BATTERY 6547 MISSIONS ( ampbfll {'egg WITH HIGH CONCENTRATIONS IAC-12.C2.4.12 ALUMINIUM-SCANDIUM ALLOYHS COMPATIBILITY 6548 HYDROGEN PEROXIDE Yuuei Zhang THE MECHANICAL, THERMAL AND IAC-12.C2.4.13 EFFECT OF MAPP AS COUPLING AGENT ON 6549 INTERFAC1AL PROPERTIES OF GLASS FIBRE-PP COMPOSITE Tomjeer Rasheed IAC-12.C2.4.I4 PROPOSED MATERIALS FOR Z-PINCH PULSE-POWERED FUSION SYSTEMS FOR 6550 SPACE PROPULSION Mitc hell Rodriguez IAC-I2.C2.4.15 MATERIALS SELECTION FOR NEUTRON REFLECTORS IN NUCLEAR FUSION 6554 REACTOR SYSTEMS Mitchell Rodriguez 6559 IAC-12.C2.4.16 MATERIAL AND SURFACE PROPERTIES OF LARES SATELLITE Antonio Paolozzi

IAC-I2.C2.4.17 THERMAL PROTECTION TECHNIQUE ADVANCE IN RESEARCH OF HYPERSONIC 6566 VEHICLE SHARP LEADING EDGE Ai Hang Cheng IAC-12.C2.4.18 DESIGN STRATEGIES FOR SPACE SYSTEMS AND SUBSYSTEMS USING ADVANCED NANO-MATERIALS AND MANUFACTURING TECHNOLOGIES 6567 Athunaxiox Baltapoulox IAC-I2.C2.4.I9 THE EFFECTS OF STACKING SEQUENCE OF THE SKIN UPONTHE DELAMINATION GROWTH PROCESS FOR COMPOSITE ADVANCED GRID STIFFENED STRUCTURES (AGS) 6568 Jin Yu

IAC-12.C2.4.20 NUMERICAL INVESTIGATION ON CONDUCTION-COOLED SUPERCONDUCTING MAGNETS IN SPACE 6569 Yoh Nagasaki IAC-12.C2.4.21 DEVELOPMENT OF NEW MD/FE COUPLING METHOD FOR MULTISCALE MODELING OF NANOSTRl (TI RED SPACE MATERIALS 6570 Ranafxheh Hashemi Four IAC-12.C2.4.22 CONCEPT AND MECHANICAL PROPERTIES OF BELLOWS-TYPE INFLATABLE-TUBES 6571 Himxhi Fumvu

IAC-I2.C2.4.23 DEVELOPMENT TRENDS OF MATERIALS FOR METAL SEALED STRUCTURE OF SPACECRAFT 6574 7ft- /"ti/ijr IAC-12.C2.4.24 WELDS DEFECTS IN LASER BEAM WELDED T JOINT ALUMINUM-LITHIUM ALLOY 6575 Honyhtng l.iu

C2.5. SMART MATERIALS AND ADAPTIVE STRUCTURES

IA(-12.(2.5.1 BIO-INSPIRED PROGRAMMABLE MATTER FOR SPACE APPLICATIONS 6576 ihomwi Sinn

1AC-12.C2.5.2 NOVEL KINEMATIC CONTROL TECHNIQUE FOR ELECTROACTIVE POLYMER ROLLING ROVERS 65g3 Silvio ('ocuzzo

I.\( -I2.C2.5.3 SHAPE CONTROL OF A MEMBRANE STRUCTURE WITH SHAPE MEMORY ALLOYS 6584 H\un (irxzultk IAC-12.C2.5.4 APPLICATIONS OF TUNED MASS DAMPERS TO IMPROVE PERFORMANCE OF LARGE SPACE MIRRORS 6592 Brij Agrawal 1AC-12.C2.5.5 VIBRATION CONTROL FOR MEMBRANE BY SMART DYNAMIC VIBRATION ABSORBER 6606 Shota Yamamoto IAC-12.C2.5.6 FUZZY-BASED ADAPTIVE MULTI-MODAL VIBRATION CONTROL WITH IMPERFECT STRUCTURAL DATA 6618 Kanjuro Makihara IAC-12.C2.5.7 WIRELESS STRUCTURAL HEALTH MONITORING OF SPACE STRUCTURES WITH ENERGY HARVESTING CAPABILITIES 6624 Luca Lampani IAC-I2.C2.5.8 WIRELESS STRAIN SENSING SYSTEM FOR SPACECRAFT HEALTH MONITORING 6625 Yayu Monica Hew IAC-12.C2.5.9 DESIGN OF A FIBER-OPTIC INTERROGATOR MODULE FOR THE HYBRID SENSOR BUS SYSTEM FOR TEMPERATURE MONITORING IN TELECOMMUNICATION SATELLITES 6634 Philipp Putzer IAC-I2.C2.5.10 FIBER-OPTIC STRAIN SENOR-BASED STRUCTURAL HEALTH MONITORING OF AN UNINHABITATED AIR VEHICLE 6636 Jessica Alvarenga IAC-12.C2.5.11 A DISTRIBUTED STRAIN SURVEILLANCE SYSTEM FOR CRYOGENIC TANK 6642 Peng Weibin

C2.6. SPACE ENVIRONMENTAL EFFECTS AND SPACECRAFT PROTECTION

IAC-12.C2.6.1 AEROTHERMODYNAMIC DESIGN OF SCIROCCO PLASMA WIND TUNNEL TESTS FOR IXV TPS INTERFACES 6643 Sara Di Benedeto IAC-12.C2.6.2 TRIBOLOGICAL PROPERTIES OF PTFE COMPOSITE IN LUNAR EXTREME ENVIRONMENT 6644 Koji Matsumoto IAC-12.C2.6.3 THERMAL MATERIAL EXPOSED EXPERIMENT BASED ON RVD IN LEO 6651 Jiajing Huo IAC-12.C2.6.4 ELECTROSTATIC SURFACE IN LUNAR EXPLORATIONS 6652 Nima Gharib

IAC-12.C2.6.5 THERMAL TESTS ON LARES SATELLITE COMPONENTS 6653 Antonio Paolozzi

IAC-12.C2.6.6 RADIATION SHIELDING OF COMPOSITE SPACE ENCLOSURES 6658 Garbine Atxaga IAC-12.C2.6.7 ON-GROUND TESTING METHODOLOGIES IMPROVEMENT IN ARC-JET PLASMA FACILITIES USING OPTICAL EMISSION DIAGNOSTICS 6668 A/essio Cipullo IAC-12.C2.6.8 FLIGHT EVALUATION ON SURVIVABILITY OF FEP IN SUPER-LOW EARTH ORBIT ENVIRONMENT 6678 Kumiko Yokota IAC-12.C2.6.9 ANALYSIS AND SYNTHESIS OF IMPACT RESILIENT COMPOSITE STRUCTURE USING COMPUTATIONAL SIMULATION AND COMPOSITE STRUCTURE TAILORING IN ELASTIC PANEL STRUCTURE 6683 Harijono Djojodihardjo IAC-12.C2.6.10 THE STUDY OF IRRADIATION EFFECT OF HIGH ENERGY PROTON AND ELECTRON ON TRIPLE JUNVTIONINGAP2/GAAS/GE CELL 6700 Lei Zhang IAC-12.C2.6.11 THE SIMULATION OF INTERNAL CHARGING EFFECT IN FR-4 PCB OF SATELLITE BY USING ATICS 6701 Li/ei Meng

C2.7. SPACE VEHICLES - MECHANICAL/THERMAL/FLUIDIC SYSTEMS

IAC-12.C2.7.1 RECENT THERMAL DESIGN DRIVEN DEVELOPMENT ACTIVITIES AT MT AEROSPACE 6706 Farid lnfed IAC-12.C2.7.2 CRYOGENICS TASKS IN PERSPECTIVE RUSSIAN SCIENTIFIC SPACE PROJECTS 6707 Anton Burdanov 1AC-12.C2.7.3 COATING EFFECTS ON THERMAL PROPERTIES OF CARBON CARBON AND CARBON SILICON CARBIDE COMPOSITES FOR SPACE THERMAL PROTECTION SYSTEMS 6712 Maria Albano IAC-12.C2.7.4 CHEMICAL NON EQUILIBRIUM SIMULATIONS OF HYPERSONIC FLIGHTS IN CARBON DIOXIDE-NITROGEN ATMOSPHERES USING A COUPLED EULER-SECOND-ORDER BOUNDARY LAYER METHOD 6714 Mann Starklof 6715 ROVER ON ICY MOONS OF JUPITER IAC-12.C2.7.5 RE-USE OF EXOMARS Abrur-Ul-Haq Khun Bttiui h VEHICLE: EXPERIMENTS AND EXPERT THE ESA EXPERIMENTAL RE-ENTRY IAC-12.C2.7.6 6726 FOR THE FLIGHT PAYLOADS QUALIFIED AND READY

Antonio Del Vecchio WITH SUCCESS AT LIT-INPE 6M X 8M SPACE LARGE SCIENTIFIC SATELLITE TESTED IAC-12.C2.7.7 6739 SIMULATION CHAMBER Joxe Sergio Almeida 6746 FOR HYPERSONIC FLOW SIMULATIONS IAC-12.C2.7.8 UNCERTAINTY QUANTIFICATION Jenten ('appaerl ON THE HEAT TRANSFER RATES OF A RE ENTRY 1AC-12.C2.7.9 EFFECT OF ECCENTRICITY 6747 VEHICLE WITH CONCAVE WINDWARD SURFACE tlurunadh Velidi 6749 - A PARAMETRIC STUDY 1AC -12.C 2.7.10 SOLID ROCKET BOOSTER SEGMENT JOINT Shll/i Arara BLUNT VEHICLE IAC-I2.C2.7.11 AEROTHERMODYNAMICS OF A HEMISPHERICAL-CYLINDRICAL 6755 WITH A FLOW THROUGH DUCT (iurunadh Velidi SYSTEM WITH FLEXIBLE IAC-12.C2.7.12 ROBUST NEURAL NETWORK CONTROL OFSPACE ROBOT 6762 JOINTS Zhiyong ('hell DELTA WING ROCK 6768 IAC-12.C2.7.13 EFFECT OF FOREBODY CONFIGURATION ON NONSLENDER Hing Han LOADS ON RE¬ IAC-I2.C.2.7.I4 COMPUTATIONAL ANALYSIS OF THERMAL AND STRUCTURAL AN IN-HOUSE SOLVER CODE 6769 ENTRY VEHICLES AND A CONCEPTUAL SSTO MODEL USING Shrnrup Namhiar WITH INNER FUNCTIONALLY IAC-12.C2.7.15 NUMERICAL ANALYSIS OF ENGINE CYLINDER LINER 6770 GRADED THERMAL BARRIER COATING l.ihting Yung 1AC-12.C2.7.I6 THE HUNGARIAN COCORAD EXPERIMENT IN THE BEXUS PROGRAM OF THE ESA 6771 Halazs Zabon 1AC-12.C2.7.17 AEROHEATING AND STRUCTURE COUPLED ANALYSIS IN THERMAL PROTECTION SYSTEM FOR REUSABLE LAUNCH VEHICLE 6781 Shiyong Huang IAC-12.C2.7.18 ANALYSIS OF LOAD TRANSMISSION LINE ON THE FUSELAGE OF REUSABLE LAUNCH VEHICLE 6788 Tmgtng Ma IAC-I2.C2.7.I9 SIMULATION OF MULTI-BODY SEPARATION OFAEROSPACE VEHICLES BASED ON UNSTRUCTURED OVERSET GRIDS TECHNOLOGY 6791 Zhau Liu