991 fork[1]
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1. The document proposes an optical power infrastructure in Earth-moon space using lasers powered by concentrated sunlight to distribute power virtually anywhere and anytime. 2. It identifies four technical advances needed: concentrating sunlight to saturate a laser gain medium, removing heat without distortion, exciting the lowest order laser mode, and converting laser light to electricity efficiently. 3. Experiments are proposed to demonstrate key mechanisms at small scale, with the goal of maturing the technologies to eventually enable large-scale distribution of optical power throughout the Earth-moon system.
![#4: Transform received optical power to alternative form, e.g., electrical, at high efficiencyat receiving siteLoadPV CellI
Requires matched coherentlight
()[]11lnηξξξ≅−+1kTh/ξν==
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991 fork[1]
- 1. Efficient Direct Conversion of Sunlight to Coherent Light at High Average Power in Space Richard L. Fork, Rustin L. Laycock, Dane J. Phillips, Wesley W. Walker, Spencer T. Cole, Sean D. Moultrie, John C. ReinhardtUniversity of Alabama in Huntsvilleforkr@uah.edu NASA Institute for Advanced Concepts –Phase I Report March 16, 2005
- 2. Outline Goal: Optical Power Infrastructure in Earth-moon space Methodology: Solar pumped solid state laser power oscillators most likely located primarily on the lunar surface combined with relay mirrors at L4 and L5 LaGrangian points Results: Find an Optical Power Infrastructure providing needed power virtually anywherevirtually anytimeis allowed by fundamental physical laws Conclusions: Direct attention to maturation of four technical advancesfor transforming sunlight to coherent light that are required. Could be accomplishedin time frame of exploration program.
- 3. MoonMultiple relay satellites in GEORelay satellite at L5 point Multiple distribution satellites in LEORelay satellite at L4 point MoonEarthGoal:Optical Power Infrastructure in Earth-moon space> 100 kW power virtually anywhereand virtually anytimein Earth- moon space “Energy farms” on the moon Require high average power high coherence power laser oscillators
- 4. Supply power from lunar surface to spacecraft near Earth Use of LaGrangian points provides access to regions that might otherwise be obstructed by EarthSchematic and image of optical power deliveryL5Moon Image of optical power being beamed to spacecraft near Earth Optical beams would normally not be visible in space
- 5. Schematic and image of distribution of optical power to satellites in low Earth orbit and then to Earth’s atmosphere Non-military vs. military use e.g., atmospheric monitoringArray of remotely powered economical small satellites in LEO
- 6. Delivery of coherent power safely to Earth from spaceSafety beam at low intensity surrounds power beam
- 7. Propagation distance vs. beam radius 5 m 500 m 50 m 1.0 Gm Earth-moon distance4λπ:/DL 10.0 Mm30 m384 Mm 100 Mm L e.g. liquid mirrors on moon 1.0 Mm 0.5 m Mirror diameter D(λ~1 micron)
- 8. Initial Findings •Billions of terawattsof continuously renewed clean solar power are available in Earth-moon space as sunlight •Sunlightcannot be usefully redistributed by linear optical systems •Optical power in the form of coherent light(as lowest order Gaussian modes of free space) can be distributed virtually anytime virtuallyanywhere in Earth-moon space The principal need is to transform sunlight into coherent light at high average powerat reasonableefficiency in space
- 9. Transforming sunlight into coherent light at high average powerin space requires fourtechnical advances1. Concentratesolar pump power to the saturation intensity of a useful laser transition in a gain volume approximating the lowest order Gaussian mode of a near confocal resonator2. Remove waste heatfrom the gain volume in a manner that avoids unacceptable thermally induced optical distortion and stress3. Transfer the solar pump power efficiently and selectively into the lowest order Gaussian mode of a near confocal resonator4. Transform temporally and spatially coherent lightbeamed of Earth-moon distances at high efficiency, e.g. > 90%, into alternative, e.g. electrical powerLoadPV CellI
- 10. #1: Concentrate needed solar pump power in required volume at ~ saturation intensity of laser transition, e.g. 10 kW/cm2Spectrally filtered sunlight Non-imaging concentrators Tapered duct Core doped with laser material Design determined by optimizing concentration of pump power in most favorable geometry and dimensions using Advanced Systems Analysis Program (ASAP) (Hubble)
- 11. Selective absorption in central gain material doped region Rays “bounce” in zigzag pattern, but are eventually absorbed with high probability in the gain material Achieve integratedpump intensity substantially largerthan intensity at the surface of the Sun
- 12. “Multiple suns” point of view Each concentrator contributes power to gain medium comparable to conventional concentrator16 non-imaging concentrators each concentrate sunlight to maximum intensity at a plane 3m length yields ~ 100 kW > 80% of solar pump power is ~uniformly absorbed in the core region End view1X3X Sixteen timesthe effective intensity of one concentrator
- 13. Conventional optics for 8 collector concentrator 40 m~ 5 m 25 m Estimate 4 kg/kW on basis of NASA optics Projections- comparable to nuclear projections Collecting area for 8 concentrators is 200 m2 At 1 kg/m2mass is 200 kg <1 metric ton for 200 kW output
- 14. #2: Remove heat from gain medium while avoiding thermally induced lensing and distortion200K235K230KOptical axis Heat removed axiallyfrom gain material having large thermo optic coefficient, e.g. YAG Heat removed radiallyusing material having small thermo- optic coefficient and large thermal conductivity, e.g. diamond or undoped sapphire Positivethermally induced lens is compensated by negativethermally induced lens
- 15. #3: Need large cross sectional area, e.g., 1.5 cm radius, lowest order Gaussian mode of a near confocal resonator of practical dimensions Double confocal paraboloidal resonator ~ 3 m Conventional lowest order Gaussian mode resonators would be kilometerslong
- 16. #3. Double confocal paraboloidal resonator using Brewster angle gain elements Provides low lossgain elements
- 17. #3 Double confocal paraboloidal resonator using Brewster angle gain elements Energy brought in by solar pump photons must be transferred with high probability to lowest order Gaussian mode Selective transfer to the lowest order Gaussian mode requires selective lossintroduced in the resonator
- 18. Technical advances 1,2,and 3 provide means of delivering optical power throughout Earth-moon spaceMoonMultiple relay satellites in GEORelay satellite at L5 point Multiple distribution satellites in LEORelay satellite at L4 point MoonEarth
- 19. #4: Transform received optical power to alternative form, e.g., electrical, at high efficiencyat receiving siteLoadPV CellI Requires matched coherentlight ()[]11lnηξξξ≅−+1kTh/ξν== Have neglected all sources of inefficiency except for thermal mechanisms
- 20. Cost, income, specific power vs. year CostIncome200020502025 Years $10,000kW/kg $/kg 0Specific Power1.000.5 $5,000
- 21. Current Experimental Results Ti:sapphire0 ms24 ms50 mssapphiresapphireValidates transient approach 532 nm pump Experimentally measured temperature profile in Ti:sapphire as a function of time
- 22. Plan of workEntech, Inc4.High efficiency optical to electrical3. Large area resonator with selective excitationNRL, ANL2. Removal of heat with no distortion? Nanostructured interfacesTransient pump probe experiment1. Concentration of solar pump powerPartnerTechnicaldevelopmentExperimentTASKAnalysisCompare results and simulationMeasure power concentration?Build scaled down resonator in our laser labPerform experiments on NASA diodesSample diodes to be builtCompare results and theoryParaboloidal reflectorsCompare results and predictions Build concentrator elements Laser for transient, heliostat for cw
- 23. Issues: 1.Can transient measurements provide data adequate to evaluate high cw power? Ans. Longest relevant time constants are ~10 ms, so approach has scientific validity. Only way to perform meaningful experiments within current budget.
- 24. 2. What is the case for scalingto high total power at reasonable cost? Ans. The physical phenomena allow construction of small scale system that illustrates the key mechanisms. Build small scale system and project the cost. The answers will be found in the maturing of the technologies. No obvious reason cost will be a show stopper.
- 25. 3. What would be the cost of robotic assembly in space? Ans. We can make the system elements modular. The technology is similar to that of Project Lasso now being explored.
- 26. 4. Sounds to good to be true. Ans. Coherent light is different from conventional light. One may discover capabilities that were not fully anticipated.
- 27. Conclusions 1.An optical Power Infrastructure in Earth-moon space is allowedby fundamental physical laws 2.There are fourareas of technology maturation that are required to make such an infrastructure a possible 3.The advances that are required are difficult, but are likely to yield to determined efforts. 4.The cost benefit analysis strongly recommends making the effort.
- 28. Special thanks to this years UAH laser and optics classes! Spring ’05 ST: Advanced Optics ASHMORE, SHERMAN BLAIR CHRISTENSEN, JORDAN SCOTT HANKS, JONATHAN BRAUNLILLEY, DARREN JOSEPH RHODES, JAMES MATTHEWROSE, AMANDA ANN YESKE, BENJAMIN SCOTTBOWEN, PAUL DENVA CUNEO, JASON HOWARDREINHARDT, JOHN CHARLES Fall ’04 Laser Systems HANKS, JONATHAN BRAUNRHODES, JAMES MATTHEW ROSE, AMANDA ANNSUTHERLAND, DANE RYAN VADEN, JUSTIN PARKERYESKE, BENJAMIN SCOTT ASHMORE, SHERMAN BLAIRCHRISTENSEN, JORDAN SCOTT DANIEL, ROLAND ANTHONYHUAMANI, CAROLINA MANN, MARK PAULMILLER, BRANDON JAY PRESSNELL, CHADWICK STPRESTON, GREGORY CHARLES CUNEO, JASON HOWARD WRIGHT, PATRICIA ZEORLIN BOWEN, PAUL DENVA