Presentation on theme: "Asteroid Mining Concepts Shen Ge. Near-Earth Asteroids Near-Earth Asteroids (NEAs) of interest due to the relative ease of reaching them. All NEAs have."— Presentation transcript:
Potential Products from NEAs MaterialProduct Raw silicateBallast or shielding in space Water and other volatilesPropellant in space Nickel-Iron (Ni-Fe) metalSpace structures Platinum Group Metals (PGMs)Catalyst for fuel cells and auto catalyzers Semiconductor metalsSpace solar arrays
How do we mine them? Type of MaterialProcess Water and other liquidsDrillholes. SulfurFrasch process Metals-If large, need to grind and crush them with feeders, crushers, fluid energy mills, hammer mills, etc. -If small, need to separate the metals by electrostatic or magnetic separation, sieves, carbonyl separation, or cutting.
Required Asteroid Mining System Chart from Brad R. Blair and Leslie S. Gertsch
How do we get there? We want to find the asteroids with low delta- vs to reduce propellant needed. Distribution of specific linear momentum of a Hohmann transfer from low Earth orbit (LEO) to NEAs according to Benner. 1 st WARNING: For Virgil and other non-science or engineering majors who apparently gets a headache from seeing equations, please turn your head away from the next slide.
Rocket Equation where Δv = velocity change V e = exhaust velocity M o = total mass M p = propellant mass Two Options: 1.Reduce delta-v required for trajectories to enable low-thrust propulsion methods such as electric, solar thermal, or solar sail propulsion. 2.Use chemical propulsion for high thrust trajectories if needed.
Example of a Hohmann Transfer “Apollo-Type” Mission
Interplanetary Superhighway Low delta-v trajectories combined with electric or solar propulsion can open the pathway to many more asteroids previously considered impossible to reach.
Or maybe bring the asteroid here… Diagrams from Mark Sonter Use gravity assists to bring candidates into a stable orbit around Earth or Modify orbits of temporarily- captured objects (TCOs) to make them stable orbits.
Can we justify the costs? The economic justification for an asteroid mining operation is only the case if the net present value (NPV) is above zero. It is NOT just the cost of mining and going there versus the profit obtained from resources. Sonter has done extensive work in creating a formula for these calculations. 2 nd WARNING: For Virgil and other non-science or engineering majors who apparently gets a headache from seeing equations, please turn your head away from the next slide.
Sonter’s NPV Equation C orbit is the per kilogram Earth-to-orbit launch cost [$/kg] M mpe is mass of mining and processing equipment [kg] f is the specific mass throughput ratio for the miner [kg mined / kg equipment / day] t is the mining period [days] r is the percentage recovery of the valuable material from the ore ∆v is the velocity increment needed for the return trajectory [km/s] v e is the propulsion system exhaust velocity [km/s] i is the market interest rate a is semi-major axis of transfer orbit [AU] M ps is mass of power supply [kg] M ic is mass of instrumentation and control [kg] C manuf is the specific cost of manufacture of the miner etc. [$/kg] B is the annual budget for the project [$/year] n is the number of years from launch to product delivery in LEO [years].
Expectation Value of NPV NPV should take into account the risk of failure. Exp NPV = p x NPV where p = fractional probability of outcome
The Next Steps Asteroid Composition. Create database of NEAs of interest for resource extraction with their orbits and compositions. Space Mining. Develop potential mining technologies for modified use in space. Astrodynamics. Design optimal trajectories and propulsion methods to go there and back. Space Economics. Identify costs and returns as well as potential investors.