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THE BOUNTY OF THE
     HEAVENS
        Michael Chrin
         Adam Wick
    Fifth Annual Freshman Conference, 9 April 2005
Introduction

Economics drives
and guides the path
of civilization
Growth in space
has been minimal
Launch Costs

       Reusable launch
       vehicles
        $5,000 per kilogram

       One-time rockets
        $7,000 per kilogram
Low-Cost Solutions




Image source: http://www.calpoly.edu/~rechols/astro101/astro101lab4.html
Low-Cost Solutions

               Asteroids




Image source: http://www.calpoly.edu/~rechols/astro101/astro101lab4.html
Low-Cost Solutions

               Asteroids
               Comets




Image source: http://www.calpoly.edu/~rechols/astro101/astro101lab4.html
Low-Cost Solutions

               Asteroids
               Comets
               Moon




Image source: http://www.calpoly.edu/~rechols/astro101/astro101lab4.html
Benefits of Asteroids
           Orbiting the Sun
            Proximity
            Gravity-free
            Diverse

           Millions upon
           millions exist--ready
           for the taking

               Image source: http://www.calpoly.edu/~rechols/astro101/astro101lab4.html
Asteroidal Locations




Image source: Mining the Sky [11]
Number/Size
Comparison
NEAR-Shoemaker

        Near-Earth Asteroid
        Rendezvous
        Demonstrated the
        capacity to locate
        and land on
        asteroids
Ideal Asteroid
 Provides both fuel
 and construction
 materials
 Type C
  Hydrocarbon Content

 Close to Earth
  Apollo Class
  Relatively small mass
The “Short List”


             Thousands of data
             yield only a handful
             of results




Data Source: NeoDys [5]
1988 TA


     14 August 2011
     23 November 2013
Designing the Vessels:

  Project Intrepid
Parts of Intrepid
Thruster
Orbiter
Mining Module
Design Challenge:
     Propulsion
Design Challenge:
                 Propulsion
Chemical Rocket
 Pros: High one-time thrust, proven

 Cons: Expensive, bulky
Design Challenge:
                  Propulsion
Chemical Rocket
 Pros: High one-time thrust, proven

 Cons: Expensive, bulky

Solar Sail
 Pros: Inexpensive, uses solar wind

 Cons: Low acceleration, untested in space, less
 effective farther from the sun.
Design Challenge:
                  Propulsion
Chemical Rocket
 Pros: High one-time thrust, proven

 Cons: Expensive, bulky

Solar Sail
 Pros: Inexpensive, uses solar wind

 Cons: Low acceleration, untested in space, less
 effective farther from the sun.

Nuclear Thermal Rocket (NTR)
 Pros: High multi-use thrust, can used mined
 volatiles as fuel, reducing weight.

 Cons: Requires the launch of fissionables into
Design Challenge:
                  Propulsion
Chemical Rocket
 Pros: High one-time thrust, proven

 Cons: Expensive, bulky

Solar Sail
 Pros: Inexpensive, uses solar wind

 Cons: Low acceleration, untested in space, less
 effective farther from the sun.

Nuclear Thermal Rocket (NTR)
 Pros: High multi-use thrust, can used mined
 volatiles as fuel, reducing weight.

 Cons: Requires the launch of fissionables into
NTR: TRITON

      TRI-modal capable
      Thrust Optimized
      Nuclear propulsion
      Developed by Pratt &
      Whitney
      Mission-configurable
TRITON Modes
Main Thrust
 Quick, efficient
 interplanetary travel

Low-Power
 Power plant for ship
 systems and ion drives

Thrust Augmentation
 Increase thrust for
 heavier loads
Main Thrust Mode

                  CERMET fuel form
                        Uranium dioxide-
                        tungsten matrix
                        Hydrogen is heated as
                        it passes through the
                        matrix
                        Hot hydrogen ejected
                        produces thrust

Image source: http://rocket.sfo.jaxa.jp/img/le5b1.jpg
Low-Power Mode
                                                                        At 1% capacity
                                                                        Uses helium xenon
                                                                        mixture
                                                                        Keeps reactor cool
                                                                        Generates 25-50 kW




Image source: http://www.bambam131.com/lewisclark/IonThruster1aaa.jpg
Thrust Augmentation Mode
 Liquid oxygen is
 added to hydrogen
 ejection system
 200% increase in
 available thrust.
 Similar to a jet
 fighter afterburner
Design Challenge:
      Orbiter

            Similar to NEAR-
            Shoemaker
                CCD camera
                Spectrometers
                Laser altimeter

            Pulsed Inductive
            Thruster
Design Challenge:
     Mining Module

 Completely enclosed system
 Design eliminates issues:
  Zero gravity mineral transportation
  Ejecting valuable minerals into space

 Powered by TRITON low-power
 mode
Mining
41-blade, flat disk
 Grinds though surface

Minerals enter craft
Transferred to
pressure vessel
Mineral Separation
          Solar arrays heat
          vessel to 1,300 K
          Electromagnetic
          field activated
          Gases and metals
          separated
          Sand dumped
          Process repeats
Conclusions

                      Inexpensive space
                      structures
                       Orbital Habitats
                       Science Stations
                       Interplanetary Rockets



Ad astra per aspera
Design and Assembly of an Economically-viable Near-Earth Asteroid Mining Robot

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Design and Assembly of an Economically-viable Near-Earth Asteroid Mining Robot

  • 1. THE BOUNTY OF THE HEAVENS Michael Chrin Adam Wick Fifth Annual Freshman Conference, 9 April 2005
  • 2. Introduction Economics drives and guides the path of civilization Growth in space has been minimal
  • 3. Launch Costs Reusable launch vehicles $5,000 per kilogram One-time rockets $7,000 per kilogram
  • 4. Low-Cost Solutions Image source: http://www.calpoly.edu/~rechols/astro101/astro101lab4.html
  • 5. Low-Cost Solutions Asteroids Image source: http://www.calpoly.edu/~rechols/astro101/astro101lab4.html
  • 6. Low-Cost Solutions Asteroids Comets Image source: http://www.calpoly.edu/~rechols/astro101/astro101lab4.html
  • 7. Low-Cost Solutions Asteroids Comets Moon Image source: http://www.calpoly.edu/~rechols/astro101/astro101lab4.html
  • 8. Benefits of Asteroids Orbiting the Sun Proximity Gravity-free Diverse Millions upon millions exist--ready for the taking Image source: http://www.calpoly.edu/~rechols/astro101/astro101lab4.html
  • 11. NEAR-Shoemaker Near-Earth Asteroid Rendezvous Demonstrated the capacity to locate and land on asteroids
  • 12. Ideal Asteroid Provides both fuel and construction materials Type C Hydrocarbon Content Close to Earth Apollo Class Relatively small mass
  • 13. The “Short List” Thousands of data yield only a handful of results Data Source: NeoDys [5]
  • 14. 1988 TA 14 August 2011 23 November 2013
  • 15. Designing the Vessels: Project Intrepid
  • 17. Design Challenge: Propulsion
  • 18. Design Challenge: Propulsion Chemical Rocket Pros: High one-time thrust, proven Cons: Expensive, bulky
  • 19. Design Challenge: Propulsion Chemical Rocket Pros: High one-time thrust, proven Cons: Expensive, bulky Solar Sail Pros: Inexpensive, uses solar wind Cons: Low acceleration, untested in space, less effective farther from the sun.
  • 20. Design Challenge: Propulsion Chemical Rocket Pros: High one-time thrust, proven Cons: Expensive, bulky Solar Sail Pros: Inexpensive, uses solar wind Cons: Low acceleration, untested in space, less effective farther from the sun. Nuclear Thermal Rocket (NTR) Pros: High multi-use thrust, can used mined volatiles as fuel, reducing weight. Cons: Requires the launch of fissionables into
  • 21. Design Challenge: Propulsion Chemical Rocket Pros: High one-time thrust, proven Cons: Expensive, bulky Solar Sail Pros: Inexpensive, uses solar wind Cons: Low acceleration, untested in space, less effective farther from the sun. Nuclear Thermal Rocket (NTR) Pros: High multi-use thrust, can used mined volatiles as fuel, reducing weight. Cons: Requires the launch of fissionables into
  • 22. NTR: TRITON TRI-modal capable Thrust Optimized Nuclear propulsion Developed by Pratt & Whitney Mission-configurable
  • 23. TRITON Modes Main Thrust Quick, efficient interplanetary travel Low-Power Power plant for ship systems and ion drives Thrust Augmentation Increase thrust for heavier loads
  • 24. Main Thrust Mode CERMET fuel form Uranium dioxide- tungsten matrix Hydrogen is heated as it passes through the matrix Hot hydrogen ejected produces thrust Image source: http://rocket.sfo.jaxa.jp/img/le5b1.jpg
  • 25. Low-Power Mode At 1% capacity Uses helium xenon mixture Keeps reactor cool Generates 25-50 kW Image source: http://www.bambam131.com/lewisclark/IonThruster1aaa.jpg
  • 26. Thrust Augmentation Mode Liquid oxygen is added to hydrogen ejection system 200% increase in available thrust. Similar to a jet fighter afterburner
  • 27. Design Challenge: Orbiter Similar to NEAR- Shoemaker CCD camera Spectrometers Laser altimeter Pulsed Inductive Thruster
  • 28. Design Challenge: Mining Module Completely enclosed system Design eliminates issues: Zero gravity mineral transportation Ejecting valuable minerals into space Powered by TRITON low-power mode
  • 29. Mining 41-blade, flat disk Grinds though surface Minerals enter craft Transferred to pressure vessel
  • 30. Mineral Separation Solar arrays heat vessel to 1,300 K Electromagnetic field activated Gases and metals separated Sand dumped Process repeats
  • 31. Conclusions Inexpensive space structures Orbital Habitats Science Stations Interplanetary Rockets Ad astra per aspera

Notas del editor

  1. Throughout history, economics has been the premier driving force behind the design, development, and implementation of new technologies. Because space travel is so expensive and, at this time, dangerous, progress made towards exploring and exploiting outer space has been stunted at best.
  2. Launch costs are still extremely high, despite many NASA and corporate attempts to find alternate, cheaper methods of reaching outer space. For a large payload, like that of a space station or interplanetary rocket, upwards of $500,000,000 could be spent on launches alone.
  3. Asteroids- Because they’re already *in* space, there is no need to fight earth’s gravity well. Comets- Comets are somewhat trickier to manipulate--they’re generally fussier than asteroids due to their high volatile material content. Moon- The moon has long been an object of Man’s envy. However, in mining the moon, one would be subject to being constrained to only the minerals that are on the Moon--there is little diversity. Also, fighting the Moon’s gravity well becomes an issue.
  4. Asteroids are the best choice for a primary mining operation 1. Proximity-- Many come close to the Earth in predictable orbits 2. No gravity-- No gravity means no launch costs, which in turn means cheaper spacecraft 3. Diversity--Several types of asteroids exist--some metallic, some carbonaceous, some made almost entirely of ammonia 4. sheer numbers--NASA scientists think that most asteroids in the solar system are the remains of a planet never formed.
  5. As of 1996, about 20,000 asteroids were known and tracked. 203 of them were found found to be Near-Earth Asteroids, or NEAs According to more recent research, the number of near-earth asteroids exceeds 50,000, when asteroids 100m in diameter or larger are counted. As you can see, there are quite a healthy number of asteroids for the taking.
  6. This chart shows the total number of asteroids that exist, plotted against their diameters, given in kilometers. Notice the power-law nature of this chart-- there are many *many* more small asteroids than larger ones.
  7. You might say, getting to asteroids is hard! Well, the recent NEAR-Shoemaker mission, funded by NASA, proved in 2001 that reaching asteroids is indeed possible--NEAR-Shoemaker actually “touched down” on the asteroid Eros.
  8. The best, principal choice for an asteroid mining operation is one that comes close to earth two times in a five-year period, one that will yield both fuel and construction materials, and one that has a relatively small mass. Type C, Apollo-class asteroids generally fulfill all of these requirements.
  9. THis data is curtsy of the NeoDys databank. NeoDys is maintained by the University of Pisa, in Italy. Each piece of asteroid data that has been accumulated by nationally-funded and amateur astronomers has been faithfully entered into the database, which is accessible through the internet. Although many asteroids fulfill our requirements, asteroid 1988TA does it best--it has the most optimal combination of size and orbital approaches. Finding 1988 TA was very much a chore.
  10. Here is an orbital diagram of asteroid 1988 TA. This snapshot was taken on 13 July 2011, as the the asteroid begins to approach earth. The two dates of closest approach are given on the right. As you can see, the duration of the mining operation on 1988 TA will be approximately two years in length. I will now hand the presentation over to my associate, Michael.
  11. Factors considered: endurance, expense, thrust. Nuclear Thermal are the ideal choice. Their reusability and greater thrust decreases the cost and the amount of mission time expended traveling to and from an asteroid.
  12. The Triton rocket is a type of Nuclear thermal rocket, developed by Pratt and Whitney. It uses a fast spectrum nuclear reactor. It has the unique ability to adapt to different situations, and can be used for at least 15 missions before the propulsion system needs to be replaced. *Note: v= {Fast spectrum alludes to higher energy neutrons (.1Mev)}
  13. Besides it main thrust mode, which produces a large amount of thrust over a one hour time period, the Triton rocket can operate in a low power mode which generates electricity once the rocket is heading towards its destination. The Triton also can be switched to a thrust augmentation mode to increase its thrust for heavier loads.
  14. The main propulsion system uses a CERMET fuel form, an advanced fuel based on a uranium dioxide-tungsten matrix. During operation of the TRITON engine, hydrogen is pumped through the gaps in the matrix, causing the hydrogen to become heated. The hot hydrogen gas is then ejected out of the craft producing 71,000N.
  15. The low-power mode operates by replacing the hydrogen with a mixture of helium and xenon. This mixture is heated and is then used to simultaneously produce electricity for the ship and cool the reactor. When the reactor is being used in this fashion, it uses less then 1 percent of its maximum power, and produces anywhere from 25-50 kilowatts of electricity.
  16. The thrust augmentation system operates by pumping liquid oxygen from an onboard tank directly into the hydrogen ejection system to allow the oxygen to interact with the extremely hot hydrogen gas. Because the oxygen hydrogen reaction is extremely exothermic the thrust increases by 200%
  17. The TRITON rocket is only one part the Intrepid.
  18. As the Intrepid descends to dock with the asteroid, the orbiter has been deployed, and the bow of the vessel splits apart, folding up against the sides of the craft. Once docked the mining procedure begins. The mining modual is entirely enclosed within the intrepid.
  19. Intrepid’s mining module is equipped with a 41-blade, flat-disk mining implement, to penetrate the asteroid. Intrepid will actually be able to use the essentially nonexistent gravitational environment to its advantage: the minerals mined will be free to enter the Intrepid, due to the rotational nature of the mining saws. A conveyor system, placed along the long axis of Intrepid, is made up of multiple scoops attached to a belt, allowing it to fill a portion of the interior of the craft to contain and move the materials. These minerals are then emptied into the pressure vessel.
  20. By mining 1988 TA one time, over 1.5 billion dollars worth of materials could be brought to earth orbit. These new resources would allow NASA to construct other Intrepid-class vessels in outer space, reducing costs dramatically. Eventually, large space stations and habitats will be constructed. Man can then begin to proliferate through the Solar system and the stars.