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NASA Technical Reports Server (NTRS) 20020091865: Wireless Power Transmission Options for Space Solar Power PDF

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Preview NASA Technical Reports Server (NTRS) 20020091865: Wireless Power Transmission Options for Space Solar Power

IAC-02-R.4.08 WIRELESS POWER TRANSMISSION OPTIONS FOR SPACE SOLAR POWER Mark Henley*, Seth Potter ,Joseph Howell ,and John Mankms , World Space Congress, Houston; Texas, USA Oct. 17, 2002 *Program Manager, Space Solar Power, Boeing ,**Senior Specialist, Boeing ***Manager, Advanced Space Flight Projects, NASA Marshall Space Flight Center ***Chief Technologist; Human Exploration and Development of Space, NASA HQ Abstract: Space Solar Power (SSP), combined with Wireless Power Transmission (WPT), offers the far-term potential to solve major energy problems on Earth. In this paper two basic WPT options, using radio waves and light waves, are considered for both long-term and near-term SSP applications. In the long-term, we aspire to beam energy to Earth from geostationary Earth orbit (GEO), or even further distances in space. Accordingly, radio- and light- wave WPT options are compared through a wide range of criteria, each showing certain strengths. in the near-term, we plan to beam power over more moderate distances, but still stretch the limits of today's technology. For the near-term, a 100 kWe-class "Power Plug" Satellite and a 10 kWe-class Lunar Polar Solar Power outpost are considered as the first steps in using these WPT options for SSP. By using SSP and WPT technology in near-term space science and exploration missions, we gain experience needed for sound decisions in designing and developing larger systems to send power from Space to Earth. Introduction Satellite photographs of the Earth at night are, effectively, a means of remote The demand for power on Earth is sensing for power consumption, in the growing exponentially, and associated form of electric lights. Figure 1 is a environmental consequences are composite satellite photograph showing becoming significant. In this new the entire Earth at night, lit up by our century, Space Solar Power (SSP) may current levels of power consumption (as provide a clean, safe energy source, of November, 2000). Bright areas define alleviating some of the problems we power-rich population centers, generally would otherwise expect from increasing concentrated near coastlines and nuclear and fossil fuel use. waterways (note the brightness of the Nile river in Egypt). Some of the dark regions indicate barren deserts, while others,like sub-SaharanAfrica,arewell same peak power level on Earth (1.2 populated, but power-starved. Deserted GWe). Laser-Photovoltaic wireless locations adjacent to populated regions power transmission is currently less are potential sites for future large WPT efficient (by about 50%), so a larger receiving stations. solar array area is needed to collect sunlight, and the satellite becomes much Comparison of WPT Options for Far- longer (55 km), and about half as wide. Term SSP Systems WPT is provided by a series of small laser transmitters running the entire Wireless Power Transmission uses length of the satellite. Each light beam electro-magnetic waves, rather than has a relatively small diameter, so each wires, to send energy from one location diverges relatively rapidly, but their to another. Two basic alternatives are combined energy fills a large diameter (6 being considered for power beaming: kin), dual-use photo-voltaic receiver on radio waves (microwaves) and light Earth with roughly 500 W/m2 of waves (lasers). monochromatic light. This is half the peak intensity of sunlight on Earth (~1 Radio waves are beamed in a cloud- kW/m2), but, because the WPT penetrating radio-frequency band wavelength can match the photo-voltaic reserved for Industrial, Scientific and cell's band-gap, the cell's efficiency can Medical (ISM) applications). Figure 2 be much higher (e.g., >40% vs 20% illustrates an example SSP concept using efficiency). Photovoitaic electrical the 5.8 GigaHertz ISM band; in this power output may actually be greater case, a 500 meter diameter phased array with WPT than with sunlight, even transmitting antenna directs radio waves though the sunlight is twice as powerful. from GEO to a 7.5 kilometer diameter rectifying antenna on Earth, Laser-photovoltaic WPT systems do not approximately 40,000 km away from require large transmitter apertures, so the power receiving stations. Here, a 15 same net effect (1.2 GWe on Earth) kilometer long, gravity gradient- could be provided by a large number of stabilized "backbone" carries 2.8 smaller, co-orbiting satellites. GigaWatts of power from the solar panels down to the transmitter. Figure 4 summarizes key features of a Following a wide variety of loss dual-use photo-voltaic receiver. Large mechanisms (pointing, side-bands, photovoltaic power plants in major filtering, power conversion, etc.) the deserts areas can receive & convert light system provides 1.2 GigaWatts of both directly from the Sun, and via WPT electrical power on Earth. from the SSP satellite(s). Gravity gradient-stabilized SSP satellites receive Light waves are beamed in a wavelength the most sunlight, and transmit the most which can be generated efficiently and power around 6 AM and 6 PM. Around easily transmitted through the mid-day and midnight, solar panel self- atmosphere in an optical or infra-red shadowing or cosine losses significantly "window". Figure 3 illustrates an reduce the power output. The example SSP concept using lasers, combination of ambient sunlight (which instead of microwaves, to transmit the peaks around mid-day) plus WPT illumination combinesat the terrestrial waveleng!his closeto a million times PV arrayto matchthe daily electricity larger (centimeters vs nanometers). demandpattern. Light-wave WPT allows small initial demonstrationsystemsto be madeand A satellite without gimbaled arrays tested over significant distances, further improves the match between whereasradio wave WPT requires a power output and power demand. huge leap of faith (literally and Gimbaled solar panelsare heavyand figuratively) to producean initial SSP complex,and would add only a little system. more power around mid-day and midnight. Insteadof using gimbaled RadioFrequencyInterferenceis alsoa arrays,bothsidesofrigid (notgimbaled) major drawbackfor WPT using radio solararrayscanproducepower,although waves. With so much power being the"back"sideproduceslesspowerdue produced,evena small fractionoutside to occlusion by wires, and partial the ISM band-gap can create major transmissionof sunlight through the problemsfor the usersof neighboring translucentsubstrate(e.g.,Kapton). By and harmonic radio frequency bands. placing the "back" side facing the Theadditionof filters is expectedto be morningsun(East)andthe"front" side necessary,which reduces the WPT facing the afternoon sun (West), the efficiencyandincreaseslocalheating. sateilite'spoweroutputis moreclosely matched to typical terrestrial power Radio waves, at 5.8 GHz, (or, even marketdemands,which havea higher better,at the longer wavelength2.45 peak in the afternoon than in the GHz ISM Band)canpenetratethrough morning. clouds and light rain; light waves,in contrast,areeasily stoppedby weather This typeof combinedsystemhasother phenomenon,and require a dry site, far-reachingbenefitswhencomparedto preferablyathigh altitude. Whilethere a typical terrestrial solar-photovoltaic is somelogic to placing photo-voltaic (PV) system. Typical terrestrial PV WPT receivers in desert areas(e.g., installationswouldrequireamuchlarger inexpensive, otherwise unproductive areato collectpower,and would need land),not all areasthatneedpowerare power storage systems, with large neardeserts. Powerdemandsin many conversion losses, to match the countriestendto peakwhenthe sunis electricity demand. By combiningthe bright (e.g., for summer air naturaltime-dependenotutputof direct conditioning), which correspondsto solar-PV and SSPWPT-PV systems, relativelyclearskies. NonethelessW, PT bothcanbenefit. using light from an SSPsystemmay requirealternatereceiversto makegood Significant attributesof far-term SSP useofthesystemoncloudydays. systemsfor radio-waveandlight-waves WPT are comparedin figure 5 and Somelegal issuesare raised by both discussedbelow: systems. Radio wave WPT implies some degreeof RF interference,and WPT aperturesizemustbemuch,much spectrumallocationsand power limits larger for radio waves,as the WPT may need to be re-negotiated. Light waveWPTcanbedesignedto limit the attract certain types of wildlife. Radio- intensitytosafe,uncontroversiallevels, frequency coupling may be more prone butthewordingoftreatiesrelatingtothe to transfer energy into small animals, use of beamed energy for defense whose body length is comparable to the applicationswouldneedto bereviewed wavelength. Infra-red WPT light falling carefully, to determinerelevanceand on an area over a prolonged time might ensurecompliance,whereappropriate. similarly change the localized plant growing season. Infrastructure utilization appears better for light wave WPT, considering the Efficiency is currently higher for radio- reduced land area and dual application of wave wireless power transmitters and the photo-voltaic receiver for terrestrial receivers. Light wave transmitter and solar as well as SSP-WPT applications. receiver efficiency is rapidly improving, but it is not clear whether it will ever Other kinds of dual use have been approach the efficiency of radio hypothesized for both WPT options. RF frequency transmission. The combined WPT could potentially be used for data system efficiencies expected for radio- transmission, and the land beneath wave WPT have been matured through receiving antennae could potentially be related radar and communications used to grow crops. A light-beaming applications, and are expected to be in SSP system could, hypothetically, be the range of 60-70%, when filtering used to send power to orbital transfer losses are included. For Laser-PV WPT, vehicles, or even to solar sails (in the the best we expect to achieve about 50%, very far-term). though this might be improved significantly, as the technology matures Public perception is an issue for either through SSP-related flight option. The radio frequencies suggested demonstrations. When power are within the "microwave" band, and management and distribution losses are the public tends to perceive microwaves considered, there is another impact to net as something to cook with. Similarly, efficiency (and mass) for radio-wave the public may perceive power WPT, as electricity is carried to a large transmission by light to be dangerous, central transmitter via wires that are even though the system is designed to many kilometers long. ensure safety. Both the micro-wave and light-wave intensity limits suggested are Near Term Space Flight weaker than sunlight. Demonstrations To ensure public safety (and safety of Initial applications of WPT technology the receiver from public interference or in space may use experimental vandalism), either WPT option would spacecraft. Two early flight need to be sequestered. It is unclear as demonstrations are being considered as to what effects might occur to local flora Model System Configurations for Space and fauna from long term exposure Solar Power. One concept is concept within the receiver site. One might known as a "Power Plug", or "LAMP" expect that a slightly warmer spacecaft, a -100 kWe space-based environment, with local shelter, might power beaming system whose primary mission is to supply power to it's own both lunar and Mars exploration, this solar electric propulsion system and to concept (figure 8) has been referred to as other spacecraft using WPT. A second the Lunar And Mars Power spacecraft, concept is a Lunar Lander which or LAMP. descends to a mountaintop at the moon's North or South pole, and transmits NASA and Boeing are cooperating to power to a robot operating in assess a mission that will use SSP and permanently shadowed lunar polar WPT technologies to investigate the craters. anomalous high concentration of hydrogen observed around the poles of A general view of one Power Plug the moon. Figure 9 provides an concept is illustrated in figure 6. In this overview of this mission: A solar power case, to achieve the required power level generation outpost is landed and in the near-term with minimal risk, the deployed on a high peak near the North configuration improved upon the or South Pole of the moon. The landing Integrated Energy Assembly (lEA) site is chosen carefully so that outpost which is now operating on the remains in full sunlit over many months International Space Station. Figure 7 is (or even years) as the moon rotates once a photograph of this existing power per month around it's slightly inclined system, the largest space solar power axis. Landing site selection also arrays ever built (so far). With minor considers direct, line-of-sight modifications, and using current state of communications with Earth, and local the art photo-voltaic cells, the power terrain features that might obstruct produced by the lEA can be doubled, Wireless Power Transmission. WPT while keeping many of the existing, technology is used to send a significant flight-proven structures and part of this power to a telerobotic lunar mechanisms. roving vehicle, which is then able to operate in deep dark craters that are A derivative of this experimental thought to contain ice. For example, with spacecraft could be launched on a Delta a beam of light, longer distance WPT IV-class launch vehicle to Earth escape can be achieved from a transmitter on velocity (with optional lunar gravity the lander, perhaps using small relay assist swing-by(s)) and proceed into a mirrors to redirect the beam into any trans-Mars injection trajectory using regions obstructed by local topography. solar electric propulsion (SEP). It would More detail on this mission can be found again uses SEP to enter Mars stationary in a companion paper, "Space Solar orbit, where it collects solar energy and Power Technology Demonstration for beams it to a Mars surface infrastructure. Lunar Polar Applications" (IAC-02- Because of the distance involved (17,038 R.4.04). km altitude), radio-wave WPT would require huge transmitters and receivers, Summary so laser wavelengths are anticipated for WPT, with a beam diameter on the order This discussion of Wireless Power of meters (rather than kilometers), Transmission Options for Space Solar delivering an average 10 kWe of power Power has made the following key to the surface. Because it may support observations: energy profile, which allows for better Far-term micro-wave WPT options are use of [and at receiver sites. To mitigate efficient, and beam power through weather outages, multiple receiver sites, clouds / light rain, but require large sizes in desert areas, may be necessary. for long distance WPT and a specialized receiver, a rectifying antenna or Gravity gradient-stabilized "Sun Tower" "rectenna". SSP satellites may make more sense for WPT light-waves than for microwave Far- (or intermediate-) term Laser- systems, because the receiver also Pbotovoltaic WPT options are less converts ambient sunlight into efficient, but have certain system level electricity. This additional sunlight can benefits. They allow a smooth transition correct for the cosine loss otherwise from conventional terrestrial solar power observed in power production at mid- to SSP, in part because synergistic use of day. With this WPT option, rigid SSP the same photo-voltaic receiver on Earth arrays, with both sides able to convert can convert both laser-light and sun-light sunlight to electricity, may be preferable into electrical power. The smaller to rotating (gimbaled) arrays, as the aperture size also allows smaller (lower resulting power produced on Earth can cost) initial systems. match the typical daily energy demand. Laser-Photovoltaic WPT systems open SSP and WPT technology flight new SSP architecture options. Efficiency demonstrations can enable advanced of current / near-term Laser-Photovoltaic space science and exploration in the near WPT technology would seem to indicate term. The "Power Plug" or "LAMP" higher mass, but specific power may be spacecraft and the Lunar Polar Solar competitive for laser systems, as their Power outpost are two near-term smaller apertures minimize subsystem applications that can advance technology masses for WPT and power management for far-term commercial SSP systems, and distribution. Narrow light beams while providing significant value for can also overlap to generate a "top hat" near-term applications. References Boeing, Evaluation of Alternative Space Solar Power in Space for Use on Earth, Solar Power System Architectures: Final NASA report SAIC-97/1005, Contract R___eport, Jet Propulsion Laboratory NAS3-26565, Task Order 9, April, 1997 Contract 961617 (Dec. 10, 1998) Potter, Seth D., Harvey J. WiIlenberg, Boeing, Space Solar Power End-to-End Mark W. Henley, and Steven R. Kent. Architecture Study: Final Report, NASA Architecture Options for Space Solar Marshall Space Flight Center Contract Power, High Frontier Conference XIV, NAS8-98244 (Jan. 15, 1999) Space Studies Institute, May 6, 1999 Dickinson, R.M., "Beamed microwave Potter, S., Willenberg, H., Henley, M., power transmitting and receiving and Kent, S. Science Mission subsystems radiation characteristics," opportunities Using Space Solar Power JPL Publication 80-11, June 15, 1980 Technology, IAF-99-R.3.07, 50th IAF Congress, Oct. 1999, Amsterdam, The Glaser, Peter, Davidson, Frank, and Netherlands Katinka Csigi. Solar Power Satellites: A Space Energy System for Earth (1998) Takeda, Kazuya, and Kawashima, Nobuki, "Development of a Diode Laser Hoffert, Martin I., and Potter, Seth D., Energy Transmission System Model to "Energy and Information From Orbit: the Moon Pole Ice Investigation Rover", Technologies for the Greenhouse Eighteeenth ISAS Space Energy Century," in Solar Power Satellites: A Symposium; pp. 38-42, February 16, Space Energy System for Earth, edited 1999 (note: paper is written in Japanese, by Peter Giaser, Frank Davidson, and abstract in English). Katinka Csigi (1998). Kawashima, Nobuki; The Importance of McSpadden, J. O., Fan, L. and Chang, Development of a Rover for the Direct K. "Design and experiments of a high- Confirmation of the Existance of Ice on conversion-efficiency 5.8-GHz the Moon, in Transactions of the Japan rectenna," IEEE Trans. Microwave Society for Aeronautical and Space Theory Techn., vol. 46, no. 12, pp. 2053- Sciences, May, 2002, v. 43, n. 139, pp. 2060, Dec. 1998 34-35 Moore, Taylor, Renewed Interest in Williams, M.D., De Young, R.J., Space Solar Power, EPRI Journal, pp. 6- Schuster, G.L., Choi, S.H., Dagle, J.E., 17, Spring, 2000 Coomes, E. P. Antoniak, Z. I., Bamberer, J. M., Bates, J. M., Chiu, M. NASA, Final Proceedings of the Solar A., Dodge, R. E., and Wise, J. A., Power Power Satellite Program Review, Conf- Transmission by Laser Beam from 800491 July 1980 Lunar-Synchronous Satellite; NASA Technical Memorandum 4496, NASA, Space Solar Power: A Fresh November, 1993 Look at the Feasibility of Generating 0 0 0 ==I _m tO 0 0 __lJo-. "_mmm tO _ 0 _ _ 0 _N 0 z = "0 ;> _" 0 r_ I i Z I I 7"i i--- 313 -_ ml 0 0 -_ :_" Cl [D ,-,- _- oooo3 < CD < .._ CD O0 33o _o :5- C) 0 _ 73 _ 0 0 0 0 0 0 ,.< r_ (1) CD CD 3 3 .__ ._k 77 GO 0 0 0 C3" _- o Cj 3 0 c Go 0 "C3 0 ,-,- GO i==I= _m 0 GO j,._. 5 U) 0 3 m :3-

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