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Team Member. Stephen Hu Deployment Vehicle Selection Helicopter Design Hours Worked: 98. Helicopter Design. Introduction General Characteristics Constraints Deployment Conclusions Recommendations. 2. Introduction. Investigation of the surface and lakes of Titan VTOL capability
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Team Member Stephen Hu Deployment Vehicle Selection Helicopter Design Hours Worked: 98 Stephen Hu
Helicopter Design • Introduction • General Characteristics • Constraints • Deployment • Conclusions • Recommendations Stephen Hu 2
Introduction • Investigation of the surface and lakes of Titan • VTOL capability • Dependable performance in hostile environments • Able to last four months under constant operation
Constraints • Environment • Temperature • Wind • Solar Energy • Atmospheric Density • Volume/Storage • Diameter of Heat Shield • Airship Storage Stephen Hu
General Characteristics Vehicle: Helicopter Type: Coaxial Number of Blades per rotor: 2 blades Airfoil: NACA 0012 Stephen Hu
Deployment • Post-Airship Separation • Generator startup • Freefall rotor startup • Heat Shield separation Stephen Hu
Mass and Power Constraints Stephen Hu
Blade Radius vs. Power Required Stephen Hu
Forward Velocity vs. Power Required Stephen Hu
Conclusions Stephen Hu
Recommendations • More in-depth aerodynamic design • Materials • Payload • Deployment Stephen Hu
References • "The Vertical Profile of Winds on Titan." www.nature.com. 8 Dec. 2005. Nature: International Weekly Journal of Science. <http://www.nature.com/nature/journal/v438/n7069/full/nature04060.html>. • Wright, Henry S. Design of a Long Endurance Titan VTOL Vehicle. Georgia Institute of Technology. <https://wiki.umn.edu/pub/titanedd/deployment/vtol_design_paper.pdf>. • Leishman, Gordon. Principles of Helicopter Aerodynamics. Cambridge UP, 2006. Stephen Hu