UPC TEAM Ferran Casulleras Gisela Detrell Sergio Mainar Miguel Angel Villarejo Meritxell Viñas Didac Zorita Miquel Sureda (prof.)

2 May, 2008Google Lunar X Prize UPC Team Since MoonCat won GLXP our company reached…

3 May, 2008Google Lunar X Prize UPC Team Radio control moon-rovers, and take personal pictures. Send people’s ashes to the Moon. Safe enterprise data. Record advertisements & entertainment films from the Moon. We are the first company to…

4 May, 2008Google Lunar X Prize UPC Team Public & private enterprises. Google Earth 3.0 Martian missions, earth orbiters, … MoonCat technology have been used for…

5 May, 2008Google Lunar X Prize UPC Team Polithical respect and non invasive procedures. Environmental ecology (no rubish!). Moon well-looking & topology must be conserved And all that taking into account…

6 May, 2008Google Lunar X Prize UPC Team With espectacular profit-making…

7 May, 2008Google Lunar X Prize UPC Team We have not done it. But we will!!!!! Back to reality…

8 Fund Raising Google Lunar X PrizeUPC Team

9 Fund Raising May, 2008Google Lunar X Prize UPC Team Total cost: 150 M $ needed!!

10 WE NEED LOTS OF MONEY… May, 2008Google Lunar X Prize UPC Team Marketing

11 Fund Raising May, 2008Google Lunar X Prize UPC Team Preliminar Design (≈30%) Time Total Mission Cost 150 M$ Sponsoring for publicity (equipment) Individual donations, receiving exclusive pictures & information s in exchange Sponsors: Advertisement in our mission

12 Fund Raising May, 2008Google Lunar X Prize UPC Team Preliminar Design (≈30%) Detailed Design (≈50%) Time Total Mission Cost 150 M$ Venture Capitalist (Ownership of our company)  49% Bank Credit

13 Fund Raising May, 2008Google Lunar X Prize UPC Team Preliminar Design (≈30%) Detailed Design (≈50%) Construction (≈20%) Time Total Mission Cost 150 M$

14 May, 2008Google Lunar X Prize UPC Team Technical Aspects

15 Mission Parameters May, 2008Google Lunar X Prize UPC Team Possible Launchers (that reach our requirements) Falcon 9 (principal partner)Ariane5 (fiabilitity and European Technoloy)

Reaching the Moon! 2. LEO orbit1. Launch 3. LTI 4. LLO 5. Lunar Descent Orbit

5.Deceleration 6.Ejection

Landing 4 cameras on the edges Bouncing effect

19 May, 2008Google Lunar X Prize UPC Team Lunar landing site Landing on the Lunar Equator: Advantages - Safer - Earth View -Type of Landing -Solar Power Availability

20 May, 2008Google Lunar X Prize UPC Team Deployment process - Airbag deinflation - Tethraedron opening

21 May, 2008Google Lunar X Prize UPC Team De la Terre à la Lune ! ROVER (15 Kg, 200W) - 2 antennas - 2 arms with 4 cameras (3D) - 6 wires - Solar Arrays + Batteries TETRAHEDRON (50 Kg, 240W) - 3 antennas (1 parabolic + 2 Dipole) - 4 arms (for edge) with 8 cameras (3D) - Solar Arrays + Batteries - in Future with Thermic Energy

Data (900 MHz) Video (2,4 GHz) Data+Video (18 GHz) 22 May, 2008Google Lunar X Prize UPC Team

23 On the Surface of the Moon: Mobility and Mooncast ! Google Lunar X PrizeUPC Team

24 Spacecraft Technical Aspects May, 2008Google Lunar X Prize UPC Team ConceptBasic Information Spacecraft MassTotal Launch Mass: 1700 Kg Fuel Mass: 1500 Kg of fuel StructuresPrimarily Aluminum. (Some titanium, berylium and composites) Avarage power requirement Rover: 200W Tetrahedron: 240 W Solar arrays & batteries Attitude Control3-axis stabilized Thermal controlHeaters, radiators & heat pipes PayloadTetrahedron: 50 kg Rover Mass: 15 kg Extra mass: 500g Rocket EngineR-40A Isp=310s Bipropellant N2O4/MMH

Thank you for your attention Ferran Casulleras Gisela Detrell Sergio Mainar Miguel Angel Villarejo Meritxell Viñas Didac Zorita Miquel Sureda (prof.)