Kite launch using an aerostat Ir. J. Breukels Delft University of Technology Faculty of Aerospace Engineering The Netherlands ________________________________________________________________________ 1 Kite launch using an aerostat Ir. J. Breukels ASSET Chair Faculty of Aerospace Engineering Delft University of Technology, the Netherlands Kluyverweg 1 2629HS Delft The Netherlands Tel: 0152585571
[email protected] Delft, August 21st 2007 ________________________________________________________________________ 2 Table of contents Table of contents 3 Nomenclature 1. Introduction 5 2. Requirements 6 2.1 Operational requirements 6 2.2 Docking and release requirements 6 2.3 Ground handling requirements 6 2.4 Safety requirements 6 2.5 Meteorological requirements 7 3. The aerostat 7 3.1 Operating the aerostat 9 3.2 Aerostatics 9 3.3 Aerodynamics 10 4. The kite release system 13 4.1 Chin docking 13 4.2 Piggy-back docking 14 5. Kite and aerostat combined 16 6. Observations during testing 16 6.1 July 25th 2007 16 6.2 July 26th 2007 17 6.3 August 14th 2007 17 6.4 August 17th 2007 17 7. Conclusions and recommendations 18 References 19 ________________________________________________________________________ 3 Nomenclature B - The upward buoyancy force acting on a body Cd - Drag coefficient Cf - Friction coefficient d - Diameter of the aerostat Df - Friction drag Dp - Preddure drag Ld - Disposable or net lift Lg - Gross or total buoyancy lift of the enclosed gas Re - Reynolds number Swetted - Wetted surface of the body V - Volume W - Total weight of the system W0 - The weight of the envelope ρa - Air density of the local atmosphere ρg - Air density of the internal gas volume ________________________________________________________________________ 4 1.