Book of Abstracts for the 4:th CEAS Conference, 2013

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(1)Cover art pictures are NASA DLR/Thilo Kranz Saab AB (publ). the copyright of: Public Domain, 2013 (CC-BY 3.0), 2013 All Rights Reserved, 2013. The individual papers are Copyright of their respective authors.. Book of Abstracts for the 4:th CEAS Conference, 2013. Editors: Tomas Melin Petter Krus Emil Vinterhav ¨ Knut Ovreb¨ o. Link¨ opings Universitet Link¨ opings Universitet SCC ECAPS SAAB AB. Place of publ.: Link¨ oping Publisher: Link¨ oping University Electronic Press Printed by: Link¨ oping University LiU-Tryck 581 83 Link¨ oping SWEDEN ISBN: 978-91-7519-520-9 First Edition, September 2013..

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(3) Book of Abstracts of the 4:th CEAS conference, Link¨oping 2013 Editors: Tomas Melin Petter Krus Emil Vinterhav ¨ Knut Ovreb¨ o.

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(5) CEAS2013. iii. Introduction. Welcome We welcome you to the fourth CEAS (Council of European Aerospace Societies) Air and Space Conference. We have chosen the theme ’Innovative Europe’ for the gathering of Europe’s most qualified professionals in air and space technologies. Europe has a leading role in research, engineering and manufacture of aerospace systems. Today, development of new concepts and systems are increasingly dependent on cooperation and mutually beneficial relationships, such that meetings and networking between professionals become even more important. Those are the basics for this conference, and the necessary elements for the air and space industries of Europe to take innovative and leading steps into the future. We are very happy to have received so many high quality contributions in such a wide range of topics. We are also proud to have a number of very high profile keynote speakers and thematic sessions with invited speakers, to reflect the overall theme of the conference. There are contributions from more than twenty countries, also from outside of Europe. Integrated in this conference are also a great number of national contributions in line with our regular national conference on aviation and space technologies. We feel confident that this range of presentations will firmly establish the CEAS Air & Space conference as one of the most important events among the community of air and space professionals. The city of Link¨ oping has a background of more than one hundred years in aviation, and is the locus of many emerging companies in the air and space arenas. Additionally, Link¨ oping is situated in a beautiful rural district with many lakes, channels and rivers. The city was founded in the 12th century and is the fifth largest city in Sweden, where you can find many places and buildings of historical interest. We wish you a fruitful meeting and a pleasant stay in Link¨ oping.. Petter Krus Chairman of programme committee Professor in Fluid and Mechatronic Systems, Link¨ oping University. Roland Karlsson Chairman of the organizing committee Chairman of the Swedish Society of Aeronautics and Astronautics.

(6) CEAS2013. iv. Introduction. Some words from the program secretary This document is the collection of abstracts of papers and presentations held at the CEAS2013 conference. They are a mix of academic papers and industrial presentations, joining the 4:th CEAS air and space conference with Flygtekniska f¨ oreningens Flygteknik Congress 2013. At the submitting to press the final presentation program was not yet fixed, meaning no index of presentation slots could be given. However, the abstracts herein are ordered after topic. Papers numbers of papers that have been withdrawn after printing will be posted at the conference. Abstracts are listed in the index section, sorted on page number, paper number and first author name. Full papers for the academic contributions will be available in the proceedings after the conference. I would personally like to thank all authors who have worked hard and submitted their work to this conference, thereby helped making CEAS2013 an endeavour of the highest quality.. Dr. Tomas Melin, program secretary.

(7) CEAS2013. v. Page Index. Papers sorted by page number. Page Paper # 1 2. Author. 167. 3. 28. 4. 202. 5. 273. 6. 37. 7. 15. 8 9. 135 161. 10. 265. 11. 124. 12. 14 T.Fransson. 13. 60 C. Grillo. 14. 12 C. Hermans. 15. 206 L.J. Johnston. 16. 49 M.K. Jung. 17 18. 109 M. Kamii T .D. 261 Kothalawala. 19. 44 A. Krzysiak. 20. 10 A.Kwiek. 21. 176 S. Micheál. 22. 163 C.J. O’Reilly. 23. 138 E. Otero. 24. 41 R. Putzu. 25. 219 M. Righi. 26. 179 C. Schmidt. 27 28. 69 S Schweikert 3 G. R. Seyfang. 29. 144 V.P. Shorin. 30. 57 D. Simon. 31 32. 111 W. Stalewski 137 M. Tomac. 33. 177 P. Weinerfelt. 34 35. Title. Numerical Simulation of Weapons Bay Store Separation Aeroacoustic research at GKN Aerospace Engine M. Billson Systems The role of optimization tools in a real-life wing design T. Bråmå with aeroelastic contraints CFD sensitivity analisys on bumped airfoil P. Caso characteristics for inflatable winglet Mission adaptive wing-let optimization for reducing F M Catalano vortex drag FLUID-STRUCTURE INTERACTION ANALYSES OF WINGS WITH CURVED PLANFORM: PRELIMINARY M. R. Chiarelli AEROELASTIC RESULTS Autofocus and adaptivity for wavelength-resolution P. Dammert airborne SAR systems Experimental Study on Aerodynamic Characteristics of H.T. Endo Ornithopter N.Fabrizio Wind tunnel tests of a new commuter aircraft effects of roll maneuver on unrestrained aircraft S. A. Fazelzadeh wing/stores flutter experimental aircraft system identification from flight A. Fedele data: procedures and results.. 46 T. Berglind. 84 S. Wiggen 136 M. Zhang. Datainsamling i ett distribuerat avioniksystem Flight Control Research Laboratory Unmanned Aerial System flying in turbulent air: an algorithm for parameter identification from flight data Innovations in wind tunnel testing to ensure competitiveness at DNW High-Lift and Radar Cross Section Characteristics of Unmanned Combat Air Vehicles Employing Serrated Leading-Edge Strakes Numerical Investigation of Aerodynamic Interaction for a Quad-Rotor UAV Configuration Experimental Analysis on Dynamic Characteristics of an Ornithopter THE INFLUENCE OF GROUND PROXIMITY ON THE AERODYNAMICS OF A WHEEL An Experimental Study of a Separation Control on the Wing Flap Controlled by Close Loop System Study on the influence of deflected strake on the rocket plane aerodynamic characteristics. Experimental/Numerical Investigation of the Mean and Turbulent Characteristics of a Wingtip Vortex in the Near-Field. Keywords Internal weapon bay stores separation, simulation, CFD, flight mechanics Propulsion, Jet noise, Aeroacoustics, CFD, transonic shock oscillation Aeroelastic optimization tools Aerodynamics, inflatable wing, CFD sensitivity to bumped airfoil Aero design, morphing winglet, optimization, mission adaptive Aerodynamics, novel planform, reduce wave drag, aeroelastics, flutter analysis Sensor - SAR data processing method, test & sim , NFFP Ornithopter, Aero characteristics, experimental Aero, WT test of new commuter concept Aerodynamics, Roll manouver effects of external stores, flutter Parameter identification from flight data, FLARE ultralight Dataregistrering för DIMA arkitektur (Gripen E), underhåll, planering Parameter identification from flight data, turbulent air, UAS Experimental Aero - WT, DNW -Large Low Speed upgrades UVAC RCS and high lift characteristics, serrated strake Aerodynamics, time accurate, unsteady flow CFD, interaction, multi-rotor UAV ornithopter (flapping wing), reentry capsule application (space oe aero session??) Aerodynamics, ground proximity, landig gear wheel, CFD Experimental Aero, WT, separation control by blown flap, closed loop control Aero: Vortex flow on re-entry vehicle. Aerodynamics, wing tip vortex modelling and investigation Aeroacoustics, CFD, transonic shock An Investigation into Shock Oscillation Noise Reduction oscillation Increasing the Efficiency of the CFD code Edge by LUSGS Aero CFD, EDGE improvements Design and construction of a silent wind tunnel for aeroacoustic research Experimental Aero, WT, aeroacoustics Aerodynamics, turbulence modelling, compressible flow, gas-kintic schemes Gas-kinetic schemes for compressible turbulent flow rather than NS A Simple Laboratory Approach to Investigate Boundary Aerodynamics, boundary layer transition, Layer Transition due to Free Stream Particles NLF, lab experiment cooling of High temp materials, re-entry Aero-Thermal Behaviour of Actively Cooled Porous vehicles, combustion chambers, porous C/C Structures by Means of Transpiration Cooling carbon/carbon structures Micro T-strips to save cost and fuel Aerodynamics, L/D increase Propulsion, measurement of pressure Acoustic probes for pressure pulsation measurement in pulsation in turbine and combustor, gas turbine flow duct and combustor methods, sensors, software Nmodel Predictive Control - MPC in aero optimal control for flight control law design & FCS design Computational design and investigations of closedloop, active flow control systems based on fluidic devices, improving a performance of wing high-lift Aerodynamics, high lift, fluidic active flow, systems. CFD & control steps towards automated robust rans meshing Aero CFD, RANS automated meshing Aerodynamic Optimization of Control Surface Control surface schedule, optimization, Schedules for Trim on the New Gripen Aircraft Aerodynamics, CFD, Fighter Development of an unsteady wind-tunnel experiment Exprimental Aero, WT, UCAV flying wing for vortex dominated flow at a Lambda – wing planform Aerodynamic Shape Design for a Morphing Wing with Aero design, morphing wing, regional a/c, Wingtip of a Regional Jetliner FP7 NOVEMOR.

(8) CEAS2013. vi. Page Index. Papers sorted by page number. Page Paper #. Author. 36. 156 R. F. de Oliveira. 37. 129 J.Aaltonen. 38. 158 L.C. Akoto. 39. 127 V. Alarotu. 40. 42 43. 122 L. Bougas Raghu 182 Chaitanya.M.V Raghu 183 Chaitanya. M. V 97 S. CHIESA. 44. Pier Davide 199 Ciampa. 41. 45. 64 S. Deinert. 46. 146 C. Galiński. 47. 233 C. Jouannet. 48 49. 11 V. A. Komarov M. C. 23 Leijonhufvud. 50. 155 A Malm. 51. 200 Pengfei Meng. 52. 211 E. Moreira. 53. 257 A. Steiz. 54. 655 Z. Wang. 55 56. 65 Z. Wang 194 Örjan Festin. 57. 29 J. Christensen. 58. 216 Håkan Forsberg. 59. 143 P.P. García. 60. 56 H. Hellsten. 61. 61 Bo Leijon. 62. 186 Rongbing Li,. 63. 267 N. Petre. 64. 240 A. Bettella. 65. 250 D. Cariolle. 66 67. 253 A. Chanoine 260 U. Gotzig,. 68 69. 75 A. Hetem 181 J. Jain. Title In-flight emergency flight planning using a decoupled trajectory optimization technique Combined Virtual Iron Bird and Hardware-in-the-Loop Simulation Research Environment for Jet Fighter Hydraulic Systems Process for Evaluation and Validation of Non-Original Components for Aircraft Hydraulic Systems on the estimations of backlash in high-lift drivetrains Aircraft Hydraulic Fluid On-Line Condition Monitoring System for Maintenance and Troubleshooting Purposes Propulsion integration and flight performance estimation for a low observable flying wing demonstrator RAPID - Robust Aircraft Parametric Interactive Design Integrated Aircraft Design Network about feasibility of a 5th generation light fighter aircraft Preliminary Design for Flexible Aircraft in a Collaborative Environment Aeroelastic Tailoring Through Combined Sizing and Shape Optimization Considering Induced Drag The Concept of the Joined Wing Scaled Demonstrator Programme Aircraft Conceptual Design Optimization Based on Direct Simulation Multidisciplinary Aircraft Design Software in Aeronautical Education Confident aircraft design and development using robust aeroelastic analysis Challenges with the transfer of aircraft production in an offset business Modeling for Physics Based Aircraft Predesign in a Collaborative Environment An Application of AHP, TOPSIS-Fuzzy and Genetic Algorithm in Conceptual Aircraft Design Parametric Design Studies for Propulsive Fuselage Aircraft Concepts. Keywords Trajectory optimization, emergency flight replanning, control, flight mechanics, performance. Simulation of fighter hydraulics, iron bird, HILS (F/A-18) Actuation, high-lift drivetrain. Improved simulation model with shaft mass Maintenance, Monitoring & Diagnostics, Hydraulic fluid & hyd. System, (F/A-18 test object) UCAV stealth propulsion integration & performance, conceptual design Conceptual design, knowledge based tool, RAPID, multidisciplinary Conceptual design, network, knowledge based, RAPID Conceptual Design, 5th gen fighter Collaborative structural, conceptual design, flexible aircraft, aeroelasticity, CPACS Aero design, aeroelastic tailoring Concept, joined wing, scaled demonstrator Concept design optimization, multidisciplinary, linked modules, UCAS Education, Multidisc. A/C design software - WINGOPT Structural design & analysis, stores, aeroelasticity. Production transfer in offset business Collaborative design, conceptual, multidisciplinary, CPACS Conceptual design, aircraft, fuzzy logic and genetic algorithms Concept, Flightpath 2050, new propulsive system, aircraft configuration Conceptual design of reentry vehicle, Conceptual design of aerospace plane the next decade space shuttle weight analysis method of hot wing for Weight Analysis of Hot Structures reentry vehicle, space shuttle Vision system supported manufacturing and repair of Composites, manufacturing and repair, aircraft composite structures vision systems for quality control Next Generation Radio Occultation Instrument for Weather Forecasting and Climate Research Space - sensing weather and climate Use of Next Generation Complex COTS in Avionics Avionics, COTS, next generation, Requires Extensive Multi-Disciplinary Skills certification, safety, architecture, skill Magnetometer Calibration Method for Small Calibration Dataset Navigation, magnetometer calibration Miniaturized Foliage Penetration Radar: Technology, Sensor, CARABAS VHF/UHF foliage Testing and New Developments penetration, improvements Sensor, product presentation, AIRTRACER – an airborne SIGINT solution COMINT/SIGINT/ELINT design of a small air data and MEMS INS/GPS integrated navigation system for wing-in-ground effect vehicles Navigation, Air Data, MEMS INS/GPS Modeling and numerical simulation of an open-loop miniature capacitive accelerometer for inertial Navigation, INS, modelling and simulation navigation applications of aceclerometer Hybrid Rockets as a green replacement of solid rocket Propulsion, Green hybrid rockets for UAV boosters for UAV assisted take off assisted takeoff Space, Propulsion, solid rocket plume, Dispersion and chemical composition of SRM rocket chemical composition, modelling and plumes: measurement Space, Life Cycle Assessment, Eco LCA for Environmental Impact Assessment of Space design tool for space missions Non-Toxic Propellants for Space Propulsion Space, non-toxic propellant Veson: a family of small sounding rockets. Simulations Simulation of sounding rocket, HOPSAN, with Hopsan Education Risk Assessment and Analysis of Disposal and Reentry of Space Debris Space debris, reentry risk assessment.

(9) CEAS2013. vii. Page Index. Papers sorted by page number. Page Paper #. Author. Title Multidisciplinary approach for assessing the atmospheric impact of launchers Deorbiting of spacecraft at the end of life with electrodynamic tethers stabilized by passive oscillation dampers. 70. 48 A.D. Koch. 71. 47 R. Mantellato. 72. 266 M. Nikulainen. 73. 101 J. Olsson. 74. 248 M. Saint-Amand. 75. 134 M. De Santis. 76. 178 M.Scheper. 77. 255 M.Smith. ASTRIUM Space Transportation environmental impact assessment of space sector_28022013 Space Debris Removal from LEO – Controlled ReEntry using an OTV / Space-Tug vs. De-Orbit Packs ESA Investigation of Additive Manufacturing for Propulsion. 78. 254 M.Smith. ESA Green Propulsion Activity - Abstract for Presentation in Clean Space Sessions. 79. 252 T. Soares. 80. 116 B. B. Virgili. 81. 245 P. Voigt. 82. 259 W. Welland. 83. 100. 84. 198. 85. 191. 86 87. 196 140. 88. 173. 89. 102. 90. 30. 91. 148. 92. 210. 93. 223. 94. 227. 95. 230. 96. 224. 97. 205. 98. 71. 99. 164. 100. 174. 101. 236. The ESA Clean Space Materials, Processes and EEE Components Increased Propellant Throughput for 1N Green Rocket Engine. LCA for Environmental Impact Assessment of Space Criteria for the Selection of Targets for Active Debris Removal Astrium perspective on space debris mitigation & remediation De-orbit motor for nanosatellites based on solid propulsion. Keywords Atmospheric emissions/polution in rocket launch, modelling and assessment Satellite deorbition by passive light system and Lorentz forces Space, environmental aspects of materials, processes, electrical components Green rocket engine, ADN Space, Propulsion, Life cycle assessment rocket motorcase, clean space Space, Life cycle assessment, ESA Space debris removal from LEO, Space tug Space, propulsion, green additive manufacturing, ESA Space, propulsion, green propellants, needs, priorities, issues, ESA strategy & roadmap Space, Life cycle assessment of European launch vehicles, ESA, environment Space, active debris removal criterias Space debris, LEO, prevention, avoidance, survivability,. Space debris removal, de-orbit motor Biofuel, green propellant for rocket engine, N.Wingborg High performance green propellants solid, liquid hybrid ADN, Ad hoc Collaborative Design with Focus on Iterative Collaborative design, multidisciplinary, Achim Multidisciplinary Process Chain Development applied thermal management of spacecraft, Basermann, to Thermal Management of Space Crafts conceptual design Conceptual, Collaborative design, Collaborative understanding of disciplinary correlations multidisciplinary/MDO, knowledge based, Erwin Moerland using a low-fidelity physics based aerospace toolkit correlations, "re CRESCENDO" FAS4Europe, EDA study, required Katarina technology and capability for future air Bjorklund FAS4Europe, what happened then power in Europé, joint with all industries K. Johansson Military demonstrator projects at GKN Aerospace Propulsion, GKN Military demonstrators JTI Clean Sky, TE - Tech Eval, Model A. Junior Clean Sky Technology Evaluator (TE) mission, airport, ATS GKN Aerospace in the Clean Sky demonstrator R. Lundberg programme Clean Sky, SAGE & SFWA Challenges in national and international R&T EU FP7 LOCOMACHS - lean production, M.Weiland collaboration projects. GF Demo (SWEDEN) Collaborative multipartner development, Collaborative multi-partner modelling & simulation M&S, Behaviour Digital Aircraft BDA, EU E.H. Baalbergen processes to improve aeronautical product design FP6 CRESCENDO, MBSE Adson Agrico de Education, Aeronautical engineering, Paula A Case Study in Aeronautical Engineering Education design aerodynamics, pedagogics Investigation of multi-fidelity and variable-fidelity Collaborative design, aircraft, variable optimization approaches for collaborative aircraft fidelity optimization, multidisciplinary, J. Jansen design CPACS, conceptual Cristina Cost optimization with focus on reliability and system System safety, reliability, early design, Johansson safety tradeoff, optimization, genetic algorithms Education, student aircraft concept, C. Jouannet Personal jet, a student project demonstrator Propulsion, nuclear power concept, BWB, Feasibility study of a nuclear powered blended wing EU FP7 RECREATE, in-flight docking, G. La Rocca body aircraft for the Cruiser/Feeder concept cruiser/feeder Collaborative design, CPACS, Virtual Aircraft Multidisciplinary Analysis and Design Multidisciplinary analysis & design, Processes - Lessons Learned from the Collaborative evaluation & LL: MDO tools OK, but Björn Nagel Design Project VAMP collaborative enginering teams a challenge Application of CAD/CAM/CAE Systems to the Process reverse engineering on thin walled of Aircraft Structures Analysis by Means of Reverse structures to yield algorithms to identify A. Olejnik Engineering Methods loads Conceptual aircraft design with hybrid laminar flow Conceptual design, passenger A/C, HLF, K. Risse control MICADO software Collaborative Aircraft Design, distributed Collaborative Aircraft Design using AAA and CEASIOM engineering, concept, multidisciplinary, "re A. Rizzi linked by CPACS Namespace CRESCENDO" Open Access Publishing in Aerospace – Opportunities Knowledge, sharing, online aerospace D. Scholz and Pitfalls journals, cooperation amongst nations.

(10) CEAS2013. viii. Page Index. Papers sorted by page number. Page Paper #. Author. 102. 226 R. van Dijk. 103. 264 D. Zafirov. 104 105. 21 P. C. Vratny Goetzendorf190 Grabowski. 106. 104 F. Asadi. 107. 32 J.Block. 108 109 110 111. 4 G.A. Di Meo 165 M. Elfving 96 ? Erlandsson 92 C. Grillo. 112. 207 Sander Hartjes. 113. 142 H.H. Hesselink. 114. 58 J. Holmberg. 115. 175 J Jeppson. 116. 85 L.Larsson. 117. 238 J. Linde. 118. 237 J. Linde. 119. 201 Amina Malik. 120. Francesca 221 Matares. 121. 42 P.G. Matei. 122. 123 124. 114 T. Melin. 18 M.Micallef 263 R. Mori. 125. 68 U. Ohlander. 126. 38 A. Popov. 127. 162 E.Ressner. 128. 45 L. Rundqwist. 129. 180 D.-R. Schmitt. 130 131. 19 Zoran Sjanic 90 K.Straube. 132 133 134. 51 J. Wallin Henric 225 Andersson 27 M. Carlsson. 135. 171 R. DENIS. 136. 187 Fir Ingo Staack. Title Knowledge-Based MDO for next generation design systems UAV Joined Wing Testbed BATTERY PACK MODELING METHODS FOR UNIVERSALLY-ELECTRIC AIRCRAFT Comparison of traditionally calculated stability characteristics with flight test data of PW-6U sailplane Route Optimization for Commercial Formation Flight Using PSO & GA Using Monte Carlo Simulation as Support for Decision Making while Negotiating a PBL Contract: A Case Study of the Saab 105 aircraft fleet SESAR and Military Aircraft: Human Machine Interface definition for 4D Trajectory Management and ASAS Spacing functionalities Enhanced methods for geometric and photometrical alignment when projecting in domes Decision Support for Future Fighter Aircraft Automatic Landing System for Civil Unmanned Aerial System Terminal Route Optimization for Cumulative Noise Exposure Innovative airport and ATM concept (operating an endless runway) Integration Aspects of a Tactile Display in a Fighter Cockpit Early assurance of Gripen E combat performance ? Effect on fuel consumption when flying to avoid formation of persistent contrails. Keywords Collaborative design, MDO, Knowlede based, design optimization UAS concept, joined wing, demonstrator testbed Battery Propulsion 2035 - modelling & opimization Stability and control, predictions, flight test comparison, glider Route optimization, formation flight, commercial, modelling, algorithms, optimization. Logistics simulation. HMI, 4D-trajectory, SESAR & Military Simulator, visualization, dome projector alignment HMI, Decision support Civil UAS Autoland system, ground effect, mainly aero & flight dynamics Trajectory optimization, noise, modelling ATM concept, innovative airport, EU FP7, ACARE 2050, circular runway HMI, tactile vest tested in simulator, Pilot feedback, FoT FTEK10-12 Operational capability evaluation, Gripen E (Next Gen), tactical simulation in OpVal. Fuel consumption, contrails, environment HMI, Night Vision in Gripen, development Integration of ANVIS in the JAS39 fighter aircraft and flight test field service of the swedish reconnaissance capability Operation, Libya, field service and support in operation unified protector of reconaissance capability Concept Assessment for Remotely Piloted Commercial UAS commercial, backup pilot on ground, Aircraft using Multi-Attribute Nonlinear Utility Theory RPV, concept assessment DORATHEA: AN INNOVATIVE SECURITY RISK ATM, security enhancement, risk ASSESSMENT METHODOLOGY TO ENHANCE assessment methodology, EU SECURITY AWARENESS IN ATM DOROTHEA pilots’ performance optimizing: dual approach – lateral Pilot performance model for student component of virtual flight and physiological profiling candidate selection, HMI, physiological, Validation of a numerical simulation tool for aircraft Formation flight simulation tool, Tornado formation flight. VLM, Towards Optimised Profile Descents at Malta International Airport through Revised Approach Procedures Trajectory optimization, approach, ATM Optimal Spot-out Time – Taxi-out Time Saving and ATM, airport simulation, taxi-out, departure Corresponding Delay management Enhancing Situation Awareness with a Large Area Display HMI, large display for fighters The Russian Federation airspace structure analysis with the use of ATM research simulation tool ATM simulation Air operations, mission planning, geospatial intelligence, augmented reality, Geospatial Intelligence for Air Operations AI, data security UCAV autonomy and collaboration, ETAP Unmanned collaborating autonomous aircraft 5.1, European 3-nation led by SW Demonstration of Satellites Enabling the Insertion of UAS traffic insertion C2 BLOS COMM via Remotely Piloted Aircraft Systems in Europe satellites, simulation, demonstration Fusion of Information from SAR and Optical Map SAR and Map Image - fusion for Images for Aided Navigation navigation a new safety net for tower runway controllers ATM, ATC, SESAR Maintenance, Monitoring & Diagnostics, The Servitisation of the Aerospace Industry and the method and tools for PSS - Product Affect on its Product Development Service Systems Gripen Core; an aircraft simulator family based on M&S, model reuse, simulator family, MBD, model reuse and customer adaptation Air vehicle systems, Model storage (Core) Enabling Uncertainty Quantification of Large Aircraft System Simulation Models MBSE - uncertainties PRESAGE : VIRTUAL TESTING PLATFORM APPLICATION TO THRUST REVERSER ACTUATION M&S, Virtual testing, mechatronics, thrust SYSTEM reverser Integration of On-Board Power Systems Simulation in Conceptual design, power systems Conceptual Aircraft Design simulation, hydraulics, 6DOF, HOPSAN.

(11) CEAS2013. ix. Page Index. Papers sorted by page number. Page Paper #. Author. 137. 217 Richard Avellán. 138. 275 S.Bagassi. 139. 105 F. Cleopatra. 140. 270 C. R. D’cruz. 141. 91 L. Ellbrant. 142. 35 F.G. Florean. 143. 98 A. Herbertz. 144. 33 O. Hultgren. 145. 166 C. Jeßberger. 146. 53. 147. 145. 148. 168. 149. 94. 150. 204. 151 152. 79 243. 153. 242. 154. 113. 155. 151. 156. 203. 157. 119. 158. 160. 159. 246. 160. 141. 161. 70. 162. 88. 163. 192. 164. 215. 165. 39. 166. 214. 167 168. 43 125. 169. 126. 170. 78. 171. 52. 172. 31. 173. 152. 174. 117. Title Boxprop, a forward swept joined-blade propeller DEVELOPMENT OF A PRELIMINARY DESIGN METHOD FOR HYBRID PROPULSION Novel Pulse Detonation Engine Concept Numerical Criterion to Optimize the Performance of a Gas Turbine Combustor Set-based compressor design method accounting for efficiency and stability LIF experiments in a turbulent reactive flow using an afterburner C*-Efficiency Evaluation of Transpiration Cooled Ceramic Combustion Chambers Bio Jet Fuels for Military Applications & Space Plugand-Play Avionics Sustainable Alternative Fuels for Aviation: International Emission Targets vs. Sustainability Aspiration. Keywords Propulsion, joined blade propeller, sfc, open rotor, aerodynamics Concept aircraft, hybrid power, preliminary design method Propulsion, pulse detonation engine, rotating combustor cans Propulsion, gas turbine combustor, optimization, CFD, emission Engine, Compressor design, CFD Propulsion, visualization of hot gases in afterburner flameholder, Laser Space, rocket engine combustion chamber cooling, ceramics BioFuel, Propulsion, environment. Biofuel, target 2050, emissions CFD of each engine component, coupled A. V. Krivcov Coupled CFD simulation of gas turbine engine core into an engine core model Transonic compressor flutter research within the Propulsion, transonic compressor flutter, H. Mårtensson FUTURE project EU FP FUTURE Efficiency improvement of a multistage compressor by Propulsion, CFD optimization, compressor V.N. Matveev optimization stagger angles of blade rows blades Numerical simulations of two-phase turbulent reactive Egine, gas turbine combustion chamber, A. C. Petcu flows NS, 3D RANS, Aero simulation Constantin Numerical evaluation of combustion chamber Propulsion, combustion chamber, CFD Rotaru performances for an aircraft engine evaluation A unified method of identification and optimization of Geometric definition of aero-surfaces S. Zietarski airfoils for aircrafts, turbine and compressor blades. rather than aerodynamic analysis P.Bodin The Attitude and Orbit Control System on Solar Orbiter Space, attitude and orbit control, ESA Space, formation flying, rendevous, P.Bodin The PRISMA Formation Flying Mission Mango/Tango spacecraft Feasibility study of small satellites launcher vehicle Space, small aircraft launched satellite A. D’Ottavio launched from atmospheric carrier aircraft launchers Space, navigation, guidance system, A. Helmersson Guidance Systems for Sounding Rockets rockets, historic development Time-Triggered Ethernet communication in launcher Space, new avionics for ethernet databus T. Hult avionics communication Environmental impact assessment of the PROBA2 Space, life cycle assessment of satellite J. Leijting satellite environmental impact. Space, Single Stage to Orbit reusable Longstaff Skylon D1 Performance launcher, SKYLON D1, REL/ESA FROM SMART-1 to ELECTRA - THE IMPLEMENTATION OF ELECTRIC PROPULSION IN Space, electric propulsion, SMART-1 to P. Rathsman SPACE ELECTRA A. L. Rodriguez- Magnetic Satellite Attitude Control: analysis of ASRE Vazquez design method under perturbations Space, Satellite attitude control Structure, buckling and modal analysis, D. Abajo buckling_and_modal_analysis_of_rotationally_restrained_orthotropic_plates plates with stringers, ribs, skins Turbine high temp superalloys, modelling R. Brommesson Modelling of the cyclic behaviour of superalloys of dynamics Rodrigo de Sá Structural design, tensegrity truss Martins Tensegrity Structures for Aircraft Applications structure, Development of heat resistant composite structures Structure, heat resistant composites, aeroPatrik Fernberg within collaborative project SHEFAE engines, surface heat exchangers Robust design, variation, geometric assurance tools with CFD and FEM A.Forslund Uncertainties in Early Phases of Aerostructure Design simulation, early phases Torbjörn M. a cost efficient 3d permeability measurement method Structure and materials, composite Green for composite manufacturing manufacturing method Structural design, conceptual, lighter and E. Holmberg Topology optimization w.r.t. stress and fatigue faster Jakobsson GKN weldability Superalloy weldability Detailed modeling of low velocity impact on a hybrid laminated composites damage simulation, Z. Kapidzic wing box structure FE, delamination Variable Fidelity Loads Process in a Multidisciplinary Loads analysis in multidisciplinary, R. Liepelt Aircraft Design Environment preliminary design High temperature hold time fatigue crack growth E. Lundström behaviour of Inconel 718 High temp materials, fatigue crack growth Topology design of a metallic load introduction bracket W. Machunze manufactured by ALM 3D printer, structure Studies on manufacturing-related management Production, strategy, Management, A. Myrelid accounting manufacturing and accounting relationship Direct-hit development of manufacturing processes: Thermo-mechanical forming of Titanium aero engine Propulsion, titanium engine structures E.-L. Odenberger structures manufacturing.

(12) CEAS2013. x. Page Index. Papers sorted by page number. Page Paper #. Author. 175. 256 M. Oliver. 176. 139 R. Olsson. 177. 40 R. Pederson. 178. 108 M. REMBECK. 179. 50 A. Rosell. 180. 153 T. Sjöberg. 181 182 183. 59 K. Thörnblad 154 M. Thuswaldner 87 J.Vallhagen. Title A400M Aeroelastics and Dynamic Tests Strength of non-crimp fabric composites under multiaxial loads – modelling and testing The relationship between alloying elements and properties for titanium alloys Ti-6Al-4V and Ti-6Al-2Sn4Zr-2Mo A combined numerical and statistcal approach to crack propagation modeling and prediction of crack propagation rates Swedish and European research collaboration in simulation supported POD Calibration and validation of material models for containment simulation and design Efficient production of aircraft engine components using an innovative scheduling procedure Anisogrid technology made available for the west - a cooperation between RUAG, KTH and CRISM Robust Design and DFM-methodology for aerospace engine components System for lifetime assessment of laser welded titanium component Fatigue Crack Propagation with Peridynamics: a sensitivity study of Paris law parameters. Keywords Structural design, aeroelastic, & dynamic testing of A400M, wake vortex model, Structure, composite strength, modelling and testing. Titanium alloys, hot temp materials Structure, modelling & predicting crack propagation, numerical and statistical approach Non-destructive testing, simulation and evaluation of probability of detection, FP7, NFFP6 Propulsion, modelling containment, simulation and design, validation Production in multtask cell with 5 subtasks, optimized scheduling Structure, low weight grid, space application, Russian technology to west. Design for manufacturing, producability, NFFP5. 184. 66 H. Wirdelius. 185. 218 M. Zaccariotto. 186. 197 Markus Kunde. 187 188 189 190. 302 304 303 301. 191. 500 K.K. Sairajan,. Advantages of an Integrated Simulation Environment The effect of Engine Dimensions on Supersonic Aircraft Performance Cost Efficient Advanced Leading Edge Structure MIDCAS: The European Detect & Avoid project Around the World with a Solar Powered Aircraft Validation of finite element models of satellite structures. 192. 300 L. Souza. Application of the mixed H2/H00 Method to Design the Micro satellite, Rubust control, Uncertainty Microsatellite Attitude control system. model.. A.Abdalla C. Altkvist Johan Pellebergs H.Ross. NDT, model for inspection (NDE), NFFP Structure, fatigue crack propagation model Collaborative development, aircraft conceptual design, multidisciplinary integrated simulation, "re CRESCENDO".

(13) CEAS2013. xi. Paper Index. Papers sorted by paper number. Page Paper # 28. 108. Author. 3 G. R. Seyfang. 4 G.A. Di Meo. 20. 10 A.Kwiek. 48. 11 V. A. Komarov. 14. 12 C. Hermans. 12. 14 T.Fransson. 7. 15 P. Dammert. 123. 18 M.Micallef. 130. 19 Zoran Sjanic. 104 49. 21 P. C. Vratny M. C. 23 Leijonhufvud. 134. 27 M. Carlsson. 3. 28 T. Bråmå. 57. 29 J. Christensen. 90. 30 M.Weiland. 172. 31 W. Machunze. 107. 32 J.Block. 144. 33 O. Hultgren. 142. 35 F.G. Florean. 6. 37 M. R. Chiarelli. 126. 38 A. Popov. 165. 39 A.Forslund. 177. 40 R. Pederson. 24. 41 R. Putzu. 121. 42 P.G. Matei. 167. 43 E. Holmberg. 19. 44 A. Krzysiak. 128. Datainsamling i ett distribuerat avioniksystem Autofocus and adaptivity for wavelength-resolution airborne SAR systems Towards Optimised Profile Descents at Malta International Airport through Revised Approach Procedures Fusion of Information from SAR and Optical Map Images for Aided Navigation BATTERY PACK MODELING METHODS FOR UNIVERSALLY-ELECTRIC AIRCRAFT Confident aircraft design and development using robust aeroelastic analysis Enabling Uncertainty Quantification of Large Aircraft System Simulation Models The role of optimization tools in a real-life wing design with aeroelastic contraints Next Generation Radio Occultation Instrument for Weather Forecasting and Climate Research Challenges in national and international R&T collaboration projects. Topology design of a metallic load introduction bracket manufactured by ALM Using Monte Carlo Simulation as Support for Decision Making while Negotiating a PBL Contract: A Case Study of the Saab 105 aircraft fleet Bio Jet Fuels for Military Applications & Space Plugand-Play Avionics LIF experiments in a turbulent reactive flow using an afterburner FLUID-STRUCTURE INTERACTION ANALYSES OF WINGS WITH CURVED PLANFORM: PRELIMINARY AEROELASTIC RESULTS The Russian Federation airspace structure analysis with the use of ATM research simulation tool. Uncertainties in Early Phases of Aerostructure Design The relationship between alloying elements and properties for titanium alloys Ti-6Al-4V and Ti-6Al-2Sn4Zr-2Mo Design and construction of a silent wind tunnel for aeroacoustic research pilots’ performance optimizing: dual approach – lateral component of virtual flight and physiological profiling Topology optimization w.r.t. stress and fatigue An Experimental Study of a Separation Control on the Wing Flap Controlled by Close Loop System. 71. 47 R. Mantellato. 70. 48 A.D. Koch. 16. 49 M.K. Jung. Unmanned collaborating autonomous aircraft Numerical Simulation of Weapons Bay Store Separation Deorbiting of spacecraft at the end of life with electrodynamic tethers stabilized by passive oscillation dampers Multidisciplinary approach for assessing the atmospheric impact of launchers Numerical Investigation of Aerodynamic Interaction for a Quad-Rotor UAV Configuration. 179. 50 A. Rosell. Swedish and European research collaboration in simulation supported POD. 132. 51 J. Wallin. The Servitisation of the Aerospace Industry and the Affect on its Product Development. 1. 45 L. Rundqwist. Title Micro T-strips to save cost and fuel SESAR and Military Aircraft: Human Machine Interface definition for 4D Trajectory Management and ASAS Spacing functionalities Study on the influence of deflected strake on the rocket plane aerodynamic characteristics. Multidisciplinary Aircraft Design Software in Aeronautical Education Innovations in wind tunnel testing to ensure competitiveness at DNW. 46 T. Berglind. Keywords Aerodynamics, L/D increase. HMI, 4D-trajectory, SESAR & Military Aero: Vortex flow on re-entry vehicle Education, Multidisc. A/C design software - WINGOPT Experimental Aero - WT, DNW -Large Low Speed upgrades Dataregistrering för DIMA arkitektur (Gripen E), underhåll, planering Sensor - SAR data processing method, test & sim , NFFP. Trajectory optimization, approach, ATM SAR and Map Image - fusion for navigation Battery Propulsion 2035 - modelling & opimization Structural design & analysis, stores, aeroelasticity MBSE - uncertainties Aeroelastic optimization tools Space - sensing weather and climate EU FP7 LOCOMACHS - lean production, GF Demo (SWEDEN) 3D printer, structure. Logistics simulation BioFuel, Propulsion, environment Propulsion, visualization of hot gases in afterburner flameholder, Laser Aerodynamics, novel planform, reduce wave drag, aeroelastics, flutter analysis ATM simulation Robust design, variation, geometric assurance tools with CFD and FEM simulation, early phases. Titanium alloys, hot temp materials Experimental Aero, WT, aeroacoustics Pilot performance model for student candidate selection, HMI, physiological, Structural design, conceptual, lighter and faster Experimental Aero, WT, separation control by blown flap, closed loop control UCAV autonomy and collaboration, ETAP 5.1, European 3-nation led by SW Internal weapon bay stores separation, simulation, CFD, flight mechanics Satellite deorbition by passive light system and Lorentz forces Atmospheric emissions/polution in rocket launch, modelling and assessment Aerodynamics, time accurate, unsteady flow CFD, interaction, multi-rotor UAV Non-destructive testing, simulation and evaluation of probability of detection, FP7, NFFP6 Maintenance, Monitoring & Diagnostics, method and tools for PSS - Product Service Systems.

(14) CEAS2013. xii. Paper Index. Papers sorted by paper number. Page Paper #. Author. 171. 52 E. Lundström. 146. 53 A. V. Krivcov. 60. 56 H. Hellsten. 30. 57 D. Simon. 114. 58 J. Holmberg. 181. 59 K. Thörnblad. 13. 60 C. Grillo. 61. 61 Bo Leijon. 45. 64 S. Deinert. 55. 65 Z. Wang. Title High temperature hold time fatigue crack growth behaviour of Inconel 718 Coupled CFD simulation of gas turbine engine core Miniaturized Foliage Penetration Radar: Technology, Testing and New Developments optimal control for flight control law design Integration Aspects of a Tactile Display in a Fighter Cockpit Efficient production of aircraft engine components using an innovative scheduling procedure Flight Control Research Laboratory Unmanned Aerial System flying in turbulent air: an algorithm for parameter identification from flight data AIRTRACER – an airborne SIGINT solution Aeroelastic Tailoring Through Combined Sizing and Shape Optimization Considering Induced Drag. 184. 66 H. Wirdelius. 125. 68 U. Ohlander. Weight Analysis of Hot Structures System for lifetime assessment of laser welded titanium component Enhancing Situation Awareness with a Large Area Display. 69 S Schweikert. Aero-Thermal Behaviour of Actively Cooled Porous C/C Structures by Means of Transpiration Cooling. 27 161. 70 D. Abajo. 98. 71 A. Olejnik. 68. 75 A. Hetem. 170. 78 R. Liepelt. 151. 79 S. Zietarski. 34. 84 S. Wiggen. 116. 85 L.Larsson. 183. 87 J.Vallhagen. 162 131. 88 R. Brommesson 90 K.Straube. 141. 91 L. Ellbrant. 111. 92 C. Grillo. 149 110 43. 94 A. C. Petcu 96 ? Erlandsson 97 S. CHIESA. 143. 98 A. Herbertz. 83. 100 N.Wingborg. 73. 101 J. Olsson. 89. 102 R. Lundberg. 106. 104 F. Asadi. 139. 105 F. Cleopatra. 178. 108 M. REMBECK. 17. 109 M. Kamii. Keywords High temp materials, fatigue crack growth CFD of each engine component, coupled into an engine core model Sensor, CARABAS VHF/UHF foliage penetration, improvements Nmodel Predictive Control - MPC in aero & FCS design HMI, tactile vest tested in simulator, Pilot feedback, FoT FTEK10-12 Production in multtask cell with 5 subtasks, optimized scheduling Parameter identification from flight data, turbulent air, UAS Sensor, product presentation, COMINT/SIGINT/ELINT Aero design, aeroelastic tailoring weight analysis method of hot wing for reentry vehicle, space shuttle NDT, model for inspection (NDE), NFFP. HMI, large display for fighters cooling of High temp materials, re-entry vehicles, combustion chambers, porous carbon/carbon structures Structure, buckling and modal analysis, buckling_and_modal_analysis_of_rotationally_restrained_orthotropic_plates plates with stringers, ribs, skins Application of CAD/CAM/CAE Systems to the Process reverse engineering on thin walled of Aircraft Structures Analysis by Means of Reverse structures to yield algorithms to identify Engineering Methods loads Veson: a family of small sounding rockets. Simulations Simulation of sounding rocket, HOPSAN, with Hopsan Education Variable Fidelity Loads Process in a Multidisciplinary Loads analysis in multidisciplinary, Aircraft Design Environment preliminary design A unified method of identification and optimization of Geometric definition of aero-surfaces airfoils for aircrafts, turbine and compressor blades. rather than aerodynamic analysis Development of an unsteady wind-tunnel experiment Exprimental Aero, WT, UCAV flying wing for vortex dominated flow at a Lambda – wing planform Effect on fuel consumption when flying to avoid formation of persistent contrails Fuel consumption, contrails, environment Robust Design and DFM-methodology for aerospace Design for manufacturing, producability, engine components NFFP5 Turbine high temp superalloys, modelling Modelling of the cyclic behaviour of superalloys of dynamics a new safety net for tower runway controllers ATM, ATC, SESAR Set-based compressor design method accounting for efficiency and stability Engine, Compressor design, CFD Automatic Landing System for Civil Unmanned Aerial Civil UAS Autoland system, ground effect, System mainly aero & flight dynamics Numerical simulations of two-phase turbulent reactive Egine, gas turbine combustion chamber, flows NS, 3D RANS, Aero simulation Decision Support for Future Fighter Aircraft HMI, Decision support about feasibility of a 5th generation light fighter aircraft Conceptual Design, 5th gen fighter C*-Efficiency Evaluation of Transpiration Cooled Space, rocket engine combustion chamber Ceramic Combustion Chambers cooling, ceramics Biofuel, green propellant for rocket engine, High performance green propellants solid, liquid hybrid ADN, Increased Propellant Throughput for 1N Green Rocket Engine Green rocket engine, ADN GKN Aerospace in the Clean Sky demonstrator programme Clean Sky, SAGE & SFWA Route optimization, formation flight, Route Optimization for Commercial Formation Flight commercial, modelling, algorithms, Using PSO & GA optimization Propulsion, pulse detonation engine, Novel Pulse Detonation Engine Concept rotating combustor cans A combined numerical and statistcal approach to crack Structure, modelling & predicting crack propagation modeling and prediction of crack propagation, numerical and statistical propagation rates approach Experimental Analysis on Dynamic Characteristics of ornithopter (flapping wing), reentry capsule an Ornithopter application (space oe aero session??).

(15) CEAS2013. xiii. Paper Index. Papers sorted by paper number. Page Paper #. Author. Title. 59. Computational design and investigations of closedloop, active flow control systems based on fluidic devices, improving a performance of wing high-lift 111 W. Stalewski systems. Feasibility study of small satellites launcher vehicle 113 A. D’Ottavio launched from atmospheric carrier aircraft Validation of a numerical simulation tool for aircraft 114 T. Melin formation flight. Criteria for the Selection of Targets for Active Debris 116 B. B. Virgili Removal Direct-hit development of manufacturing processes: Thermo-mechanical forming of Titanium aero engine 117 E.-L. Odenberger structures Environmental impact assessment of the PROBA2 119 J. Leijting satellite Propulsion integration and flight performance estimation for a low observable flying wing 122 L. Bougas demonstrator experimental aircraft system identification from flight 124 A. Fedele data: procedures and results. 125 Jakobsson GKN weldability Detailed modeling of low velocity impact on a hybrid 126 Z. Kapidzic wing box structure Aircraft Hydraulic Fluid On-Line Condition Monitoring System for Maintenance and Troubleshooting 127 V. Alarotu Purposes Combined Virtual Iron Bird and Hardware-in-the-Loop Simulation Research Environment for Jet Fighter Hydraulic Systems Process for Evaluation and Validation of Non-Original Components for Aircraft 129 J.Aaltonen Hydraulic Systems environmental impact assessment of space 134 M. De Santis sector_28022013 Experimental Study on Aerodynamic Characteristics of 135 H.T. Endo Ornithopter Aerodynamic Shape Design for a Morphing Wing with 136 M. Zhang Wingtip of a Regional Jetliner 137 M. Tomac steps towards automated robust rans meshing Increasing the Efficiency of the CFD code Edge by LU138 E. Otero SGS Strength of non-crimp fabric composites under 139 R. Olsson multiaxial loads – modelling and testing 140 K. Johansson Military demonstrator projects at GKN Aerospace A. L. Rodriguez- Magnetic Satellite Attitude Control: analysis of ASRE 141 Vazquez design method under perturbations Innovative airport and ATM concept (operating an 142 H.H. Hesselink endless runway) Magnetometer Calibration Method for Small Calibration 143 P.P. García Dataset. 29. 144. 147. 145. 46. 146. 31 154 122 80. 174 157. 40 11 168 169. 39. 37 75 8 35 32 23 176 87 160 113. 91. 148. 155. 151. 173. 152. 180. 153. 182. 154. 50. 155. 36. 156. 38. 158. 158. 160. Keywords Aerodynamics, high lift, fluidic active flow, CFD & control Space, small aircraft launched satellite launchers Formation flight simulation tool, Tornado VLM, Space, active debris removal criterias Propulsion, titanium engine structures manufacturing Space, life cycle assessment of satellite environmental impact. UCAV stealth propulsion integration & performance, conceptual design Parameter identification from flight data, FLARE ultralight Superalloy weldability laminated composites damage simulation, FE, delamination Maintenance, Monitoring & Diagnostics, Hydraulic fluid & hyd. System, (F/A-18 test object). Simulation of fighter hydraulics, iron bird, HILS (F/A-18) Space, Life cycle assessment, ESA Ornithopter, Aero characteristics, experimental Aero design, morphing wing, regional a/c, FP7 NOVEMOR Aero CFD, RANS automated meshing Aero CFD, EDGE improvements Structure, composite strength, modelling and testing Propulsion, GKN Military demonstrators Space, Satellite attitude control ATM concept, innovative airport, EU FP7, ACARE 2050, circular runway. Navigation, magnetometer calibration Propulsion, measurement of pressure Acoustic probes for pressure pulsation measurement in pulsation in turbine and combustor, V.P. Shorin gas turbine flow duct and combustor methods, sensors, software Transonic compressor flutter research within the Propulsion, transonic compressor flutter, H. Mårtensson FUTURE project EU FP FUTURE The Concept of the Joined Wing Scaled Demonstrator C. Galiński Programme Concept, joined wing, scaled demonstrator Collaborative multipartner development, Collaborative multi-partner modelling & simulation M&S, Behaviour Digital Aircraft BDA, EU E.H. Baalbergen processes to improve aeronautical product design FP6 CRESCENDO, MBSE Space, navigation, guidance system, A. Helmersson Guidance Systems for Sounding Rockets rockets, historic development Studies on manufacturing-related management Production, strategy, Management, A. Myrelid accounting manufacturing and accounting relationship Calibration and validation of material models for Propulsion, modelling containment, T. Sjöberg containment simulation and design simulation and design, validation Anisogrid technology made available for the west - a Structure, low weight grid, space M. Thuswaldner cooperation between RUAG, KTH and CRISM application, Russian technology to west. Challenges with the transfer of aircraft production in an A Malm offset business Production transfer in offset business Trajectory optimization, emergency flight In-flight emergency flight planning using a decoupled replanning, control, flight mechanics, R. F. de Oliveira trajectory optimization technique performance Actuation, high-lift drivetrain. Improved L.C. Akoto on the estimations of backlash in high-lift drivetrains simulation model with shaft mass Space, Single Stage to Orbit reusable Longstaff Skylon D1 Performance launcher, SKYLON D1, REL/ESA.

(16) CEAS2013. xiv. Paper Index. Papers sorted by paper number. Page Paper #. Author. 9. 161 N.Fabrizio. 127. 162 E.Ressner. 22. 163 C.J. O’Reilly. 99. 164 K. Risse. 109. 165 M. Elfving. 145. 166 C. Jeßberger. 2. 167 M. Billson. 148. 168 V.N. Matveev. 135. 171 R. DENIS. 88. 173 A. Junior. 100. 174 A. Rizzi. 115. 175 J Jeppson. 21. 176 S. Micheál. 33. 177 P. Weinerfelt. 76. 178 M.Scheper. 26. 179 C. Schmidt. 129 69. 180 D.-R. Schmitt. 42. 181 J. Jain Raghu 182 Chaitanya.M.V Raghu 183 Chaitanya. M. V. 62. 186 Rongbing Li,. 41. 136 105. 85 163. 187 Fir Ingo Staack Goetzendorf190 Grabowski. 191 Erwin Moerland Rodrigo de Sá 192 Martins. 56. 194 Örjan Festin. 86. Katarina 196 Bjorklund. 186. 197 Markus Kunde. 84. Achim 198 Basermann,. 44. Pier Davide 199 Ciampa. 51. 200 Pengfei Meng. 119 4 156. 201 Amina Malik 202 P. Caso 203 T. Hult. Title Wind tunnel tests of a new commuter aircraft. Keywords. Aero, WT test of new commuter concept Air operations, mission planning, geospatial intelligence, augmented reality, Geospatial Intelligence for Air Operations AI, data security Aeroacoustics, CFD, transonic shock An Investigation into Shock Oscillation Noise Reduction oscillation Conceptual aircraft design with hybrid laminar flow Conceptual design, passenger A/C, HLF, control MICADO software Enhanced methods for geometric and photometrical Simulator, visualization, dome projector alignment when projecting in domes alignment Sustainable Alternative Fuels for Aviation: International Emission Targets vs. Sustainability Aspiration Biofuel, target 2050, emissions Aeroacoustic research at GKN Aerospace Engine Propulsion, Jet noise, Aeroacoustics, Systems CFD, transonic shock oscillation Efficiency improvement of a multistage compressor by Propulsion, CFD optimization, compressor optimization stagger angles of blade rows blades PRESAGE : VIRTUAL TESTING PLATFORM APPLICATION TO THRUST REVERSER ACTUATION M&S, Virtual testing, mechatronics, thrust SYSTEM reverser JTI Clean Sky, TE - Tech Eval, Model Clean Sky Technology Evaluator (TE) mission, airport, ATS Collaborative Aircraft Design, distributed Collaborative Aircraft Design using AAA and CEASIOM engineering, concept, multidisciplinary, "re linked by CPACS Namespace CRESCENDO" Operational capability evaluation, Gripen E Early assurance of Gripen E combat performance ? (Next Gen), tactical simulation in OpVal Experimental/Numerical Investigation of the Mean and Turbulent Characteristics of a Wingtip Vortex in the Aerodynamics, wing tip vortex modelling Near-Field and investigation Aerodynamic Optimization of Control Surface Control surface schedule, optimization, Schedules for Trim on the New Gripen Aircraft Aerodynamics, CFD, Fighter Space Debris Removal from LEO – Controlled ReSpace debris removal from LEO, Space Entry using an OTV / Space-Tug vs. De-Orbit Packs tug A Simple Laboratory Approach to Investigate Boundary Aerodynamics, boundary layer transition, Layer Transition due to Free Stream Particles NLF, lab experiment Demonstration of Satellites Enabling the Insertion of UAS traffic insertion C2 BLOS COMM via Remotely Piloted Aircraft Systems in Europe satellites, simulation, demonstration Risk Assessment and Analysis of Disposal and Reentry of Space Debris Space debris, reentry risk assessment Conceptual design, knowledge based tool, RAPID - Robust Aircraft Parametric Interactive Design RAPID, multidisciplinary Conceptual design, network, knowledge Integrated Aircraft Design Network based, RAPID design of a small air data and MEMS INS/GPS integrated navigation system for wing-in-ground effect vehicles Navigation, Air Data, MEMS INS/GPS Integration of On-Board Power Systems Simulation in Conceptual design, power systems Conceptual Aircraft Design simulation, hydraulics, 6DOF, HOPSAN Comparison of traditionally calculated stability Stability and control, predictions, flight test characteristics with flight test data of PW-6U sailplane comparison, glider Conceptual, Collaborative design, Collaborative understanding of disciplinary correlations multidisciplinary/MDO, knowledge based, using a low-fidelity physics based aerospace toolkit correlations, "re CRESCENDO" Structural design, tensegrity truss Tensegrity Structures for Aircraft Applications structure, Vision system supported manufacturing and repair of Composites, manufacturing and repair, aircraft composite structures vision systems for quality control FAS4Europe, EDA study, required technology and capability for future air FAS4Europe, what happened then power in Europé, joint with all industries Collaborative development, aircraft conceptual design, multidisciplinary Advantages of an Integrated Simulation Environment integrated simulation, "re CRESCENDO" Ad hoc Collaborative Design with Focus on Iterative Collaborative design, multidisciplinary, Multidisciplinary Process Chain Development applied thermal management of spacecraft, to Thermal Management of Space Crafts conceptual design Collaborative structural, conceptual Preliminary Design for Flexible Aircraft in a design, flexible aircraft, aeroelasticity, Collaborative Environment CPACS Modeling for Physics Based Aircraft Predesign in a Collaborative design, conceptual, Collaborative Environment multidisciplinary, CPACS Concept Assessment for Remotely Piloted Commercial UAS commercial, backup pilot on ground, Aircraft using Multi-Attribute Nonlinear Utility Theory RPV, concept assessment CFD sensitivity analisys on bumped airfoil Aerodynamics, inflatable wing, CFD characteristics for inflatable winglet sensitivity to bumped airfoil Time-Triggered Ethernet communication in launcher Space, new avionics for ethernet databus avionics communication.

(17) CEAS2013. xv. Paper Index. Papers sorted by paper number. Page Paper #. Author. 150. Constantin 204 Rotaru. 97. 205 Björn Nagel. 15. 206 L.J. Johnston. 112 92 52 166 164 58. 217 Richard Avellán. 185. 218 M. Zaccariotto. 219 M. Righi. 120. Francesca 221 Matares. 93. 223 J. Jansen. 96. 224 G. La Rocca Henric 225 Andersson. 133 102 94. 226 R. van Dijk Cristina 227 Johansson. 95. 230 C. Jouannet. 47. 233 C. Jouannet. 101. 236 D. Scholz. 118. 237 J. Linde. 117. 238 J. Linde. 64. 240 A. Bettella. 153 152. 242 P.Bodin 243 P.Bodin. 81. 245 P. Voigt. 159. Virtual Aircraft Multidisciplinary Analysis and Design Processes - Lessons Learned from the Collaborative Design Project VAMP High-Lift and Radar Cross Section Characteristics of Unmanned Combat Air Vehicles Employing Serrated Leading-Edge Strakes Terminal Route Optimization for Cumulative Noise Exposure. 207 Sander Hartjes Adson Agrico de 210 Paula A Case Study in Aeronautical Engineering Education An Application of AHP, TOPSIS-Fuzzy and Genetic 211 E. Moreira Algorithm in Conceptual Aircraft Design Torbjörn M. a cost efficient 3d permeability measurement method 214 Green for composite manufacturing Development of heat resistant composite structures 215 Patrik Fernberg within collaborative project SHEFAE Use of Next Generation Complex COTS in Avionics 216 Håkan Forsberg Requires Extensive Multi-Disciplinary Skills. 137. 25. Title Numerical evaluation of combustion chamber performances for an aircraft engine. 246 P. Rathsman. 74. 248 M. Saint-Amand. 65. 250 D. Cariolle. 79. 252 T. Soares. 66. 253 A. Chanoine. 78. 254 M.Smith. 77. 255 M.Smith. Boxprop, a forward swept joined-blade propeller Fatigue Crack Propagation with Peridynamics: a sensitivity study of Paris law parameters. Keywords Propulsion, combustion chamber, CFD evaluation Collaborative design, CPACS, Multidisciplinary analysis & design, evaluation & LL: MDO tools OK, but collaborative enginering teams a challenge UVAC RCS and high lift characteristics, serrated strake Trajectory optimization, noise, modelling Education, Aeronautical engineering, design aerodynamics, pedagogics Conceptual design, aircraft, fuzzy logic and genetic algorithms Structure and materials, composite manufacturing method Structure, heat resistant composites, aeroengines, surface heat exchangers Avionics, COTS, next generation, certification, safety, architecture, skill Propulsion, joined blade propeller, sfc, open rotor, aerodynamics. Structure, fatigue crack propagation model Aerodynamics, turbulence modelling, compressible flow, gas-kintic schemes Gas-kinetic schemes for compressible turbulent flow rather than NS DORATHEA: AN INNOVATIVE SECURITY RISK ATM, security enhancement, risk ASSESSMENT METHODOLOGY TO ENHANCE assessment methodology, EU SECURITY AWARENESS IN ATM DOROTHEA Investigation of multi-fidelity and variable-fidelity Collaborative design, aircraft, variable optimization approaches for collaborative aircraft fidelity optimization, multidisciplinary, design CPACS, conceptual Propulsion, nuclear power concept, BWB, Feasibility study of a nuclear powered blended wing EU FP7 RECREATE, in-flight docking, body aircraft for the Cruiser/Feeder concept cruiser/feeder Gripen Core; an aircraft simulator family based on M&S, model reuse, simulator family, MBD, model reuse and customer adaptation Air vehicle systems, Model storage (Core) Knowledge-Based MDO for next generation design Collaborative design, MDO, Knowlede systems based, design optimization Cost optimization with focus on reliability and system System safety, reliability, early design, safety tradeoff, optimization, genetic algorithms Education, student aircraft concept, Personal jet, a student project demonstrator Aircraft Conceptual Design Optimization Based on Concept design optimization, Direct Simulation multidisciplinary, linked modules, UCAS Open Access Publishing in Aerospace – Opportunities Knowledge, sharing, online aerospace and Pitfalls journals, cooperation amongst nations field service of the swedish reconnaissance capability Operation, Libya, field service and support in operation unified protector of reconaissance capability HMI, Night Vision in Gripen, development Integration of ANVIS in the JAS39 fighter aircraft and flight test Hybrid Rockets as a green replacement of solid rocket Propulsion, Green hybrid rockets for UAV boosters for UAV assisted take off assisted takeoff Space, formation flying, rendevous, The PRISMA Formation Flying Mission Mango/Tango spacecraft The Attitude and Orbit Control System on Solar Orbiter Space, attitude and orbit control, ESA Astrium perspective on space debris mitigation & Space debris, LEO, prevention, remediation avoidance, survivability, FROM SMART-1 to ELECTRA - THE IMPLEMENTATION OF ELECTRIC PROPULSION IN Space, electric propulsion, SMART-1 to SPACE ELECTRA Space, Propulsion, Life cycle assessment ASTRIUM Space Transportation rocket motorcase, clean space Space, Propulsion, solid rocket plume, Dispersion and chemical composition of SRM rocket chemical composition, modelling and plumes: measurement Space, Life cycle assessment of European LCA for Environmental Impact Assessment of Space launch vehicles, ESA, environment Space, Life Cycle Assessment, Eco LCA for Environmental Impact Assessment of Space design tool for space missions Space, propulsion, green propellants, ESA Green Propulsion Activity - Abstract for needs, priorities, issues, ESA strategy & Presentation in Clean Space Sessions roadmap ESA Investigation of Additive Manufacturing for Space, propulsion, green additive Propulsion manufacturing, ESA.

(18) CEAS2013. xvi. Paper Index. Papers sorted by paper number. Page Paper #. Author. 175. 256 M. Oliver. 53. 257 A. Steiz. 82 67. 259 W. Welland 260 U. Gotzig, T .D. 261 Kothalawala. 18 124. 263 R. Mori. 103. 264 D. Zafirov. Title A400M Aeroelastics and Dynamic Tests Parametric Design Studies for Propulsive Fuselage Aircraft Concepts De-orbit motor for nanosatellites based on solid propulsion Non-Toxic Propellants for Space Propulsion THE INFLUENCE OF GROUND PROXIMITY ON THE AERODYNAMICS OF A WHEEL Optimal Spot-out Time – Taxi-out Time Saving and Corresponding Delay. 10. UAV Joined Wing Testbed effects of roll maneuver on unrestrained aircraft 265 S. A. Fazelzadeh wing/stores flutter. 72. 266 M. Nikulainen. 63. 267 N. Petre. 140 5. 270 C. R. D’cruz 273 F M Catalano. 138. 275 S.Bagassi. 192 190. 300 L. Souza 301 H.Ross. 187 189 188. 302 303 304. 191. 500. 54. 655. The ESA Clean Space Materials, Processes and EEE Components Modeling and numerical simulation of an open-loop miniature capacitive accelerometer for inertial navigation applications Numerical Criterion to Optimize the Performance of a Gas Turbine Combustor Mission adaptive wing-let optimization for reducing vortex drag DEVELOPMENT OF A PRELIMINARY DESIGN METHOD FOR HYBRID PROPULSION. Keywords Structural design, aeroelastic, & dynamic testing of A400M, wake vortex model, Concept, Flightpath 2050, new propulsive system, aircraft configuration Space debris removal, de-orbit motor Space, non-toxic propellant Aerodynamics, ground proximity, landig gear wheel, CFD ATM, airport simulation, taxi-out, departure management UAS concept, joined wing, demonstrator testbed Aerodynamics, Roll manouver effects of external stores, flutter Space, environmental aspects of materials, processes, electrical components Navigation, INS, modelling and simulation of aceclerometer Propulsion, gas turbine combustor, optimization, CFD, emission Aero design, morphing winglet, optimization, mission adaptive Concept aircraft, hybrid power, preliminary design method. Application of the mixed H2/H00 Method to Design the Micro satellite, Rubust control, Uncertainty Microsatellite Attitude control system. model. Around the World with a Solar Powered Aircraft The effect of Engine Dimensions on Supersonic Aircraft A.Abdalla Performance Johan Pellebergs MIDCAS: The European Detect & Avoid project C. Altkvist Cost Efficient Advanced Leading Edge Structure Validation of finite element models of satellite K.K. Sairajan, structures Conceptual design of reentry vehicle, Z. Wang Conceptual design of aerospace plane the next decade space shuttle.

(19) CEAS2013. xvii. Author Index. Papers sorted by Author/Presenter name. Page Paper #. 37 161 187 38. 39 188 133. 106 137. 91 138. 84 1 64 2. 86. 107 152 153. 40 3 162. 65 134 4 5 41 42 66. 6 43 57. 44. Author. Title Combined Virtual Iron Bird and Hardware-in-the-Loop Simulation Research Environment for Jet Fighter Hydraulic Systems Process for Evaluation and Validation of Non-Original Components for Aircraft Hydraulic Systems. Keywords. Simulation of fighter hydraulics, iron bird, HILS (F/A-18) Structure, buckling and modal analysis, 70 D. Abajo buckling_and_modal_analysis_of_rotationally_restrained_orthotropic_plates plates with stringers, ribs, skins The effect of Engine Dimensions on Supersonic Aircraft 302 A.Abdalla Performance Actuation, high-lift drivetrain. Improved 158 L.C. Akoto on the estimations of backlash in high-lift drivetrains simulation model with shaft mass Aircraft Hydraulic Fluid On-Line Condition Monitoring Maintenance, Monitoring & Diagnostics, System for Maintenance and Troubleshooting Hydraulic fluid & hyd. System, (F/A-18 test 127 V. Alarotu Purposes object) 304 C. Altkvist Cost Efficient Advanced Leading Edge Structure Henric Gripen Core; an aircraft simulator family based on M&S, model reuse, simulator family, MBD, 225 Andersson model reuse and customer adaptation Air vehicle systems, Model storage (Core) Route optimization, formation flight, Route Optimization for Commercial Formation Flight commercial, modelling, algorithms, 104 F. Asadi Using PSO & GA optimization Propulsion, joined blade propeller, sfc, 217 Richard Avellán Boxprop, a forward swept joined-blade propeller open rotor, aerodynamics Collaborative multipartner development, Collaborative multi-partner modelling & simulation M&S, Behaviour Digital Aircraft BDA, EU 148 E.H. Baalbergen processes to improve aeronautical product design FP6 CRESCENDO, MBSE DEVELOPMENT OF A PRELIMINARY DESIGN Concept aircraft, hybrid power, preliminary 275 S.Bagassi METHOD FOR HYBRID PROPULSION design method Ad hoc Collaborative Design with Focus on Iterative Collaborative design, multidisciplinary, Achim Multidisciplinary Process Chain Development applied thermal management of spacecraft, 198 Basermann, to Thermal Management of Space Crafts conceptual design Numerical Simulation of Weapons Bay Store Internal weapon bay stores separation, 46 T. Berglind Separation simulation, CFD, flight mechanics Hybrid Rockets as a green replacement of solid rocket Propulsion, Green hybrid rockets for UAV 240 A. Bettella boosters for UAV assisted take off assisted takeoff Aeroacoustic research at GKN Aerospace Engine Propulsion, Jet noise, Aeroacoustics, 167 M. Billson Systems CFD, transonic shock oscillation FAS4Europe, EDA study, required Katarina technology and capability for future air 196 Bjorklund FAS4Europe, what happened then power in Europé, joint with all industries Using Monte Carlo Simulation as Support for Decision Making while Negotiating a PBL Contract: A Case 32 J.Block Study of the Saab 105 aircraft fleet Logistics simulation 243 P.Bodin The Attitude and Orbit Control System on Solar Orbiter Space, attitude and orbit control, ESA Space, formation flying, rendevous, 242 P.Bodin The PRISMA Formation Flying Mission Mango/Tango spacecraft Propulsion integration and flight performance estimation for a low observable flying wing UCAV stealth propulsion integration & 122 L. Bougas demonstrator performance, conceptual design The role of optimization tools in a real-life wing design 28 T. Bråmå with aeroelastic contraints Aeroelastic optimization tools Turbine high temp superalloys, modelling 88 R. Brommesson Modelling of the cyclic behaviour of superalloys of dynamics Space, Propulsion, solid rocket plume, Dispersion and chemical composition of SRM rocket chemical composition, modelling and 250 D. Cariolle plumes: measurement Enabling Uncertainty Quantification of Large Aircraft 27 M. Carlsson System Simulation Models MBSE - uncertainties CFD sensitivity analisys on bumped airfoil Aerodynamics, inflatable wing, CFD 202 P. Caso characteristics for inflatable winglet sensitivity to bumped airfoil Mission adaptive wing-let optimization for reducing Aero design, morphing winglet, 273 F M Catalano vortex drag optimization, mission adaptive Raghu Conceptual design, knowledge based tool, 182 Chaitanya.M.V RAPID - Robust Aircraft Parametric Interactive Design RAPID, multidisciplinary Raghu Conceptual design, network, knowledge 183 Chaitanya. M. V Integrated Aircraft Design Network based, RAPID Space, Life Cycle Assessment, Eco 253 A. Chanoine LCA for Environmental Impact Assessment of Space design tool for space missions FLUID-STRUCTURE INTERACTION ANALYSES OF WINGS WITH CURVED PLANFORM: PRELIMINARY Aerodynamics, novel planform, reduce 37 M. R. Chiarelli AEROELASTIC RESULTS wave drag, aeroelastics, flutter analysis 97 S. CHIESA about feasibility of a 5th generation light fighter aircraft Conceptual Design, 5th gen fighter Next Generation Radio Occultation Instrument for 29 J. Christensen Weather Forecasting and Climate Research Space - sensing weather and climate Collaborative structural, conceptual Pier Davide Preliminary Design for Flexible Aircraft in a design, flexible aircraft, aeroelasticity, 199 Ciampa Collaborative Environment CPACS 129 J.Aaltonen.

(20) CEAS2013. xviii. Author Index. Papers sorted by Author/Presenter name. Page Paper #. Author. 139. 105 F. Cleopatra. 140. 270 C. R. D’cruz. 154. 113 A. D’Ottavio. 7. 15 P. Dammert. 36 92 163 45. 135. 108 109 141 8 110 9 10 11 164 56 142 58. Title Novel Pulse Detonation Engine Concept Numerical Criterion to Optimize the Performance of a Gas Turbine Combustor Feasibility study of small satellites launcher vehicle launched from atmospheric carrier aircraft Autofocus and adaptivity for wavelength-resolution airborne SAR systems. In-flight emergency flight planning using a decoupled 156 R. F. de Oliveira trajectory optimization technique Adson Agrico de 210 Paula A Case Study in Aeronautical Engineering Education Rodrigo de Sá 192 Martins Tensegrity Structures for Aircraft Applications Aeroelastic Tailoring Through Combined Sizing and 64 S. Deinert Shape Optimization Considering Induced Drag PRESAGE : VIRTUAL TESTING PLATFORM APPLICATION TO THRUST REVERSER ACTUATION 171 R. DENIS SYSTEM SESAR and Military Aircraft: Human Machine Interface definition for 4D Trajectory Management and ASAS 4 G.A. Di Meo Spacing functionalities Enhanced methods for geometric and photometrical 165 M. Elfving alignment when projecting in domes Set-based compressor design method accounting for 91 L. Ellbrant efficiency and stability Experimental Study on Aerodynamic Characteristics of 135 H.T. Endo Ornithopter 96 ? Erlandsson Decision Support for Future Fighter Aircraft 161 N.Fabrizio Wind tunnel tests of a new commuter aircraft effects of roll maneuver on unrestrained aircraft 265 S. A. Fazelzadeh wing/stores flutter experimental aircraft system identification from flight 124 A. Fedele data: procedures and results. Development of heat resistant composite structures 215 Patrik Fernberg within collaborative project SHEFAE Vision system supported manufacturing and repair of 194 Örjan Festin aircraft composite structures LIF experiments in a turbulent reactive flow using an 35 F.G. Florean afterburner Use of Next Generation Complex COTS in Avionics 216 Håkan Forsberg Requires Extensive Multi-Disciplinary Skills. 165. 39 A.Forslund. Uncertainties in Early Phases of Aerostructure Design. 12. 14 T.Fransson. 46. 146 C. Galiński. 59. 143 P.P. García Goetzendorf190 Grabowski 260 U. Gotzig, Torbjörn M. 214 Green. Datainsamling i ett distribuerat avioniksystem The Concept of the Joined Wing Scaled Demonstrator Programme Magnetometer Calibration Method for Small Calibration Dataset Comparison of traditionally calculated stability characteristics with flight test data of PW-6U sailplane Non-Toxic Propellants for Space Propulsion a cost efficient 3d permeability measurement method for composite manufacturing Flight Control Research Laboratory Unmanned Aerial System flying in turbulent air: an algorithm for parameter identification from flight data Automatic Landing System for Civil Unmanned Aerial System Terminal Route Optimization for Cumulative Noise Exposure Miniaturized Foliage Penetration Radar: Technology, Testing and New Developments. 105 67 166. 13 111 112 60 155. 60 C. Grillo 92 C. Grillo 207 Sander Hartjes 56 H. Hellsten 151 A. Helmersson. 143. 98 A. Herbertz. 14. 12 C. Hermans. 113 68. 142 H.H. Hesselink 75 A. Hetem. Keywords Propulsion, pulse detonation engine, rotating combustor cans Propulsion, gas turbine combustor, optimization, CFD, emission Space, small aircraft launched satellite launchers Sensor - SAR data processing method, test & sim , NFFP Trajectory optimization, emergency flight replanning, control, flight mechanics, performance Education, Aeronautical engineering, design aerodynamics, pedagogics Structural design, tensegrity truss structure, Aero design, aeroelastic tailoring M&S, Virtual testing, mechatronics, thrust reverser. HMI, 4D-trajectory, SESAR & Military Simulator, visualization, dome projector alignment Engine, Compressor design, CFD Ornithopter, Aero characteristics, experimental HMI, Decision support Aero, WT test of new commuter concept Aerodynamics, Roll manouver effects of external stores, flutter Parameter identification from flight data, FLARE ultralight Structure, heat resistant composites, aeroengines, surface heat exchangers Composites, manufacturing and repair, vision systems for quality control Propulsion, visualization of hot gases in afterburner flameholder, Laser Avionics, COTS, next generation, certification, safety, architecture, skill Robust design, variation, geometric assurance tools with CFD and FEM simulation, early phases Dataregistrering för DIMA arkitektur (Gripen E), underhåll, planering Concept, joined wing, scaled demonstrator Navigation, magnetometer calibration Stability and control, predictions, flight test comparison, glider Space, non-toxic propellant Structure and materials, composite manufacturing method Parameter identification from flight data, turbulent air, UAS Civil UAS Autoland system, ground effect, mainly aero & flight dynamics. Trajectory optimization, noise, modelling Sensor, CARABAS VHF/UHF foliage penetration, improvements Space, navigation, guidance system, Guidance Systems for Sounding Rockets rockets, historic development C*-Efficiency Evaluation of Transpiration Cooled Space, rocket engine combustion chamber Ceramic Combustion Chambers cooling, ceramics Innovations in wind tunnel testing to ensure Experimental Aero - WT, DNW -Large Low competitiveness at DNW Speed upgrades Innovative airport and ATM concept (operating an ATM concept, innovative airport, EU FP7, endless runway) ACARE 2050, circular runway Veson: a family of small sounding rockets. Simulations Simulation of sounding rocket, HOPSAN, with Hopsan Education.

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