Embry Riddle Milestone

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Morning presentation for student design competition.

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Embry Riddle Milestone

  1. 1. Professor: Dr. Bogdan Udrea Team Lead: Robert Latta Team Members: David Paiz Brandon Walsh-Reed Svilen Kozhuharov Mathieu Naslin Johann Schrell
  2. 2. Overview <ul><li>WP1: Sustained Funding </li></ul><ul><li>WP2: Immediate Funding </li></ul><ul><li>WP3: From the Earth to the Moon </li></ul><ul><li>WP4: Mobility and Mooncasts </li></ul>
  3. 3. Sustained Funding <ul><li>Collect materials/data in orbit via auction </li></ul><ul><li>Locate water on lunar surface </li></ul><ul><li>Material resource on lunar surface </li></ul><ul><li>Free-Return trajectory hub in lunar orbit (cycler orbit) </li></ul><ul><li>Convert lunar regolith into rocket fuel </li></ul><ul><li>Immediate contract with companies that want/need real moon data/mapping </li></ul>
  4. 4. Immediate Funding <ul><li>Form Corporation-LLC </li></ul><ul><li>Sell business plan to Venture Capitalists </li></ul><ul><li>Venture capitalists sell our ideas to Investors (Angel), who will in turn provide capital </li></ul><ul><li>Execute business plan </li></ul><ul><li>Go IPO </li></ul>
  5. 5. Immediate Funding <ul><li>“Ideas” for the LLC (Short Term) </li></ul><ul><ul><li>Logo cluster on side of CRAFT </li></ul></ul><ul><ul><li>Etch-a-sketch in lunar surface </li></ul></ul><ul><ul><li>Name engraving on Aluminum plate </li></ul></ul><ul><ul><li>Laser logo projection on lunar surface </li></ul></ul>
  6. 6. From the Earth to the Moon <ul><li>Option A – direct injection to trans-lunar trajectory (by the launcher) </li></ul><ul><ul><li>Launchers: Minotaur V or Falcon 9 </li></ul></ul><ul><li>Option B – trans-lunar injection from a GTO orbit. </li></ul><ul><ul><li>Direct Transfer and WSB </li></ul></ul><ul><ul><li>Launchers: Minotaur IV, Falcon 9, Ariane V </li></ul></ul><ul><li>Option C – trans-lunar injection from LEO </li></ul><ul><ul><li>Preferred Launcher: Falcon I </li></ul></ul><ul><ul><li>Direct Transfer and WSB </li></ul></ul>
  7. 7. From the Earth to the Moon 2 nd Stage (Retro Rocket) 1 st Stage (Out of GTO) CRAFT (Soft Landing)
  8. 8. From the Earth to the Moon <ul><li>1st stage: Delta V applied to craft to accelerate it out of GTO. Possible to use Star 13B Solid rocket booster for this operation. Required ∆V for exit: 0.67 km/sec. </li></ul><ul><li>2nd stage: Craft deceleration. Possible to use Star 13B Solid rocket booster as well for this operation. Required ∆V for deceleration: 2.5 km/sec. </li></ul><ul><li>Soft landing: Provided by Rover/Lander motors. </li></ul>
  9. 9. Mobility <ul><li>Hoberman Sphere </li></ul><ul><li>Pyramidal </li></ul><ul><li>Wheel </li></ul><ul><li>Legged/Walker </li></ul>
  10. 10. Mobility Hoberman Sphere Wheel Walker Tetrahedral
  11. 11. Mooncasts <ul><li>NASA Lunar Reconnaissance Orbiter (LRO) Communication Relay </li></ul><ul><ul><li>S-Band TX: 2.65 GHz, RX: 2.56 </li></ul></ul><ul><ul><li>Communication Rate (Max.): ~ 120 Mbps </li></ul></ul><ul><ul><li>Visibility time of LRO from Landing Site: 127s </li></ul></ul><ul><ul><li>Min. Data Rate per LRO-cycle: 117 MB/LRO-cycle </li></ul></ul><ul><ul><li>Est. Data Rate per LRO-Cycle: 1910 MB/LRO-cycle </li></ul></ul><ul><ul><li>HD data to transfer: 34837 MB </li></ul></ul><ul><ul><li>Days to transfer HD: ~ 36 hours </li></ul></ul>
  12. 12. Summary <ul><li>WP1: Sustained Funding </li></ul><ul><li>WP2: Immediate Funding </li></ul><ul><li>WP3: From the Earth to the Moon </li></ul><ul><li>WP4: Mobility and Mooncasts </li></ul>
  13. 13. Questions <ul><li>Questions and Feedback </li></ul>

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