Boek Totaal 2016

Delft University of Technology Delft Aerospace Design Projects 2016 Inspring Designs in Aeronautics, Astronautics and Wind Energy Melkert, Joris Publication date 2016 Document Version Final published version Citation (APA) Melkert, J. (Ed.) (2016). Delft Aerospace Design Projects 2016: Inspring Designs in Aeronautics, Astronautics and Wind Energy. B.V. Uitgeversbedrijf Het Goede Boek. Important note To cite this publication, please use the final published version (if applicable). Please check the document version above. Copyright Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons. Takedown policy Please contact us and provide details if you believe this document breaches copyrights. We will remove access to the work immediately and investigate your claim. This work is downloaded from Delft University of Technology. For technical reasons the number of authors shown on this cover page is limited to a maximum of 10. Delft Aerospace Design Projects 2016 Delft Aerospace Design Projects 2016 Inspiring Designs in Aeronautics, Astronautics and Wind Energy Editor: Joris Melkert Co-ordinating committee: Coordinating committee: Vincent Brügemann, Carlos Simao Ferreira, Joris Melkert, Erwin Mooij, Jos Sinke, Wim Verhagen B.V. Uitgeversbedrijf Het Goede Boek / 2016 Published and distributed by B.V. Uitgeversbedrijf Het Goede Boek Surinamelaan 14 1213 VN HILVERSUM The Netherlands ISBN 978 90 240 6014 6 ISSN 1876-1569 © 2016 - Faculty of Aerospace Engineering, Delft University of Technology - Delft All rights reserved. No part of the material protected by this copyright notice may be reproduced or utilized in any form or by any means, electronic or mechanical, including photocopying, recording or by any information storage and retrieval system, without written permission from the publisher. Printed in the Netherlands TABLE OF CONTENTS PREFACE .......................................................................................................... 1 1. THE DESIGN SYNTHESIS EXERCISE ............................................................. 3 1.1 Introduction ........................................................................................ 3 1.2 Objective ............................................................................................. 3 1.3 Characteristics of the exercise .......................................................... 4 1.4 Organization and structure of the exercise .................................... 5 1.5 Facilities .............................................................................................. 5 1.6 Course load ......................................................................................... 5 1.7 Support and assistance ..................................................................... 6 1.8 Design projects 2015-2016 ................................................................. 6 1.9 The design exercise symposium ...................................................... 7 2. MODULAR RESEARCH UAV ..................................................................... 11 2.1 Introduction ...................................................................................... 11 2.2 Concept generation ......................................................................... 13 2.3 Trade-off ........................................................................................... 15 2.4 Final design ...................................................................................... 16 2.5 Sustainability .................................................................................... 20 2.6 Business case .................................................................................... 21 2.7 Conclusions and recommendations .............................................. 21 3. HELLCAT: LOW COST MILITARY CONTAINER TRANSPORT UAV ........ 23 3.1 Introduction ...................................................................................... 23 3.2 Objectives .......................................................................................... 24 3.3 Engine selection ............................................................................... 25 3.4 Conceptual design ........................................................................... 27 3.5 Detailed design ................................................................................ 29 3.6 Sustainability .................................................................................... 32 vi DELFT AEROSPACE DESIGN PROJECTS 2016 3.7 Conclusion ........................................................................................ 32 3.8 Recommendations ........................................................................... 33 4. QUANTUM LAUNCH SYSTEM : AFFORDABLE AND SUSTAINABLE ACCESS TO SPACE ................................................................................... 35 4.1 Introduction ...................................................................................... 35 4.2 Concepts and trade-off ................................................................... 36 4.3 Detailed design ................................................................................ 37 4.4 Cost analysis ..................................................................................... 40 4.5 Sustainability strategy ..................................................................... 40 4.6 Conclusion ........................................................................................ 41 5. SALSA: FAMILY OF AEROBATIC LIGHT SPORT AIRCRAFT ...................... 43 5.1 Background ...................................................................................... 43 5.2 Project objective and design requirements .................................. 44 5.3 Market analysis ................................................................................ 45 5.4 Concept design and trade-off ........................................................ 46 5.5 Continued conceptual design ........................................................ 47 5.6 Conclusion ........................................................................................ 53 6. WIFLY – AN EMERGENCY COMMUNICATION NETWORK FOR DISASTER AREAS ..................................................................................... 57 6.1 Introduction ...................................................................................... 57 6.2 Design requirements and constraints ........................................... 58 6.3 Concept study and related trade-off ............................................. 59 6.4 Final concept design ........................................................................ 61 6.5 Conclusion ........................................................................................ 67 6.6 Recommendations ........................................................................... 69 7. STRATOSPHERIC AEROSOL GEOENGINEERING AIRCRAFT ....................... 71 7.1 Introduction ...................................................................................... 71 7.2 Mission objective ............................................................................. 72 7.3 Design drivers .................................................................................. 73 7.4 Operational concept ........................................................................ 74 7.5 Design ............................................................................................... 77 7.6 Cost .................................................................................................... 80 TABLE OF CONTENTS vii 7.7 Sustainability .................................................................................... 81 7.8 Recommendations ........................................................................... 82 7.9 Conclusion ........................................................................................ 83 8. CAPTURE A SMALL ASTEROID AND CHANGE ITS ORBIT ......................... 85 8.1 Mission statement ............................................................................ 85 8.2 Concepts studied and related trade-offs ...................................... 87 8.3 Detailed description chosen deflection method and scientific payload ................................................................................... 89 8.4 Conceptual design of the spacecraft ............................................. 92 8.5 Conclusion and recommendations ................................................ 94 9. MICRO - PAVING THE WAY FOR INTERPLANETARY CUBESAT MISSIONS ................................................................................. 97 9.1 Introduction ...................................................................................... 97 9.2 Requirements ................................................................................... 98 9.3 Mission concepts .............................................................................. 98 9.4 Mission description ....................................................................... 100 9.5 Subsystems and configuration ..................................................... 102 9.6 Sustainability .................................................................................. 104 9.7 Conclusion and recommendations .............................................

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