Photovoltaic Properties of a

Revolutionary New Solar Cell

 

Drew A. Mazurek

andrew.mazurek@yale.edu

Department of Electrical Engineering

Yale University

15 Prospect Street

New Haven, CT  06511

 

 

Abstract

 

A region of space approximately 3,200 km from the Earth's surface called the Van Allen Belt provides an ideal location for communications satellites.  It does not carry the large communications delay of the distant geosynchronous orbits, nor does it require the number of satellites needed for full Earth coverage at lower Earth orbits.  However, the Van Allen Belt is a high radiation area in which current radiation-hard solar cell technology would degrade and become useless within days.  At Yale, we have designed a novel InP drift-based solar cell with cell lifetimes expected to be in the decades under those high-radiation conditions.  Additionally, our solar cells have a high power-to-weight efficiency, reducing the cost necessary to launch the satellites into space.

 

Introduction

 

Solar cell technology has found its way into our lives in many different places.  Solar cells provide an excellent source of power in locations distant from the power grid, where constructing power plants or running transmission lines would be too costly or inefficient.  The cells themselves also have no moving parts, making them one of the lowest-maintenance power supplies available.  By being such a low maintenance, long lasting power source, solar cells are ideal for remote areas such as water pumping stations, telecommunications stations, and lighthouses.  Solar cells are also finding their way to remote villages in many countries.  For example, in Cacimbas, a South American village in Brazil, the Brazilian Energy Ministry with support from the U.S. Department of Energy is installing 50-watt solar cells on the roofs of houses to provide the homes with fluorescent lighting.

 

In their generation of power, solar cells also produce no waste.  They are extremely environmentally-friendly and are powered from the sun, our most readily available renewable energy source.  Of all the renewable energy sources, only the sun is capable of supplying more power than is currently being used.  In addition, through implementing global solar power generation, we can become less reliant on fossil fuels and other “dirty” sources of power.  The sun provides a sustainable source of power, and as more of our energy usage comes from the sun, we can begin to slow global warming and reduce pollution.

 

The above solar cells, however, may work well in terrestrial environments, but they would not survive very long in the harsh, high-radiation environment of outer space.  At Yale, we have designed a new solar cell that is optimized for outer space applications.  It is lightweight, inexpensive to manufacture, and also radiation-hard, making it ideal for use on communications satellites.  Our new solar cell, when outfitted on the satellites, will be able to withstand the high radiations encountered at orbits of 3,200 km in the Van Allen Belt.  This report provides a brief overview of our current work.

 

The report is organized as follows.  First I will provide a short and simple introduction to current solar cell technology.  After that, I will present our new InP drift-based design, followed by measurements we obtained from our solar cell.  I will then discuss the implications of our work before I conclude.

 

Current Solar Cells

 

All solar cells to date are simply pn-junction devices that operate on the principles of diffusion.  The basic idea behind solar cells is that as photons hit the cell, those possessing more energy than the band gap of the semiconductor generate hole-electron pairs.  These holes and electrons diffuse toward the metallurgical junction, crossing it when they arrive.  Once they have crossed the junction, a net positive charge appears on the p-doped side, and a net negative charge appears on the n-doped side.  When the cell is attached to an external circuit, a voltage is set up between the two sides, and current flows.

 

A measure of diffusion is the minority carrier lifetime: the average amount of time a free hole on the n-side of the junction or a free electron on the p-side of the junction can exist before it is lost to recombination.  Recombination is a process opposite to generation in which a hole and electron combine and return to the semiconductor's crystal lattice.  In well-made high-efficiency solar cells, minority carrier lifetimes are very large; for the most part, all holes and electrons created by incoming photons will have enough time to diffuse to the other side of the junction and be available as power.  However, the minority carrier lifetime is based on physical properties of the semiconductor.  Impurities in the material can add additional states which will decrease the carrier lifetimes.  Radiation damage is also another source for reduced minority carrier lifetimes.

 

As minority carrier lifetimes are diminished, more holes and electrons will recombine and be lost before they can be extracted from the cell as power.  This causes a drop in the solar cell’s efficiency.  In the zero-maintenance environment of outer space, this is unacceptable.  Solar cells must be able to last at least years, and preferably decades.  Our new drift-based design can withstand high doses of radiation and proves to be an ideal candidate for use in communications satellites at high-radiation altitudes.

 

 

 

Our Design

 

While previous solar cells have been based on diffusion to move charge carriers, our solar cell relies on drift currents established by an electric field.  For our design, we have used molecular beam epitaxy (MBE) to grow cells with a graded n+-n doping to create a strong electric field of approximately 104 V/cm.  The cell structure can be seen in Figure 1.

 

 

Figure 1:  InP cell structure

 

 

            The electric field region starts at the surface of the cell and extends 0.2 mm deep.  As hole-electron pairs are photo-generated in this region, the holes are swiftly swept to the other side of the pn-junction.  This drift field can be seen in the band diagram in Figure 2.

 

 

Figure 2:  InP cell band diagram

 

 

            Carriers moved by drift fields, as opposed to diffusion, are not affected as much by minority carrier lifetimes.  Once a hole-electron pair has been created, it will not have enough time to recombine before it is swept into the junction.  This makes our solar cell robust in high-radiation environments of outer space.  Even as the cell is damaged and minority carrier lifetimes are decreased, the cell still has an expected lifetime on the order of decades in radiations as high as 1018 1 MeV electrons/cm2 due to its drift-based design.

 

Results

 

            Figures 3 and 4 show the light and dark IV characteristics for our drift-based solar cell.  Table 1 provides the data obtained from these measurements.

Figure 3: Light and Dark IV for InP cell at 632nm

Figure 4: Light and dark IV for InP cell at 532nm

 

 

 

632 nm (red)

532 nm (green)

Ideality factor (n)

4.22

4.22

Reverse bias current (I0)

616nA

616nA

Short circuit current (Ish)

558 mA

644 mA

Open circuit voltage (Voc)

0.695V

0.710V

Fill factor (FF)

52.32%

59.67%

Spectral response

338mA/W

230mA/W

Internal Quantum Efficiency

97%

83.21%

Efficiency (h)

12.32%

10%

Table 1: Data for InP Cell

 

 

            As can be seen from the data in Table 1, our cells have an extremely high quantum efficiency.  Figure 5 shows a comparison of quantum efficiencies of various other solar cells in comparison with ours.  It is of note that our InP design has extremely high quantum efficiencies all the way from ultraviolet at 150nm to infrared at approximately 825nm.  For almost the entire ultraviolet and visible spectrum, our cell operates at quantum efficiencies above 90%!

 

Figure 5: Internal quantum efficiency vs. wavelength for various

solar cells

 

 

 

 

            We chose InP for our design for several reasons.  As was already shown, its quantum efficiency across the solar spectrum is excellent.  Figure 6 shows the amount of power absorbed for various thicknesses of solar cells.  At only 1mm thick, InP absorbs 85% of the power available from incoming photons.  This outperforms GaAs cells, which can never attain that level of absorption, and Si cells, which would require approximately 30mm thick Si to absorb the same amount of light.  Thus, our cells are gravimetric-efficient; i.e., they have a large power-to-weight ratio.

 

Figure 6: Absorbed power vs. thickness for various solar cells

 

Discussion

 

            Communications satellites are usually placed in either high geosynchronous orbits, allowing complete coverage of the Earth with only three satellites, or in lower Earth orbits, which require many more satellites.  The main drawback of placing satellites in distant geosynchronous orbits is the long communication delays incurred.  A round trip signal time for a satellite in a 35,700 km geosynchronous orbit is approximately 0.24s.  The other option of placing satellites approximately 700 km from the Earth requires many more satellites to achieve the same coverage, and is therefore more costly.

 

            An ideal location for satellites that balances the number of satellites required, signal power requirements, and communication delay is an orbit of about 3,200 km.  However, at that altitude, there is a band of heavy radiation known as the Van Allen Belt, in which even current radiation-hard silicon solar cells would last at most a few days.  Thus, to operate communication satellites in the Van Allen Belt, more robust solar cells are required that can withstand the intense radiation.  While we have not yet tested our solar cell for radiation hardness, preliminary simulations suggest that our structures will be useful for a decade even at 3,200 km polar orbits.

 

 

            Our solar cells have also been designed with a high gravimetric efficiency.  With satellite launch costs at $5,000/lb., it is obvious that satellite designers do not want the solar cells to take up a large portion of their weight budget.  The cells we have designed are lightweight and have a very high efficiency.  We have also designed them to be inexpensive to manufacture.  Current high efficiency solar cells cost $10/cm2.  Preliminary calculations estimate that our cells will be available for $1/cm2.

 

Conclusion

 

            Current solar cell technology is ill-suited to high-radiation environments.  New innovations were required to create solar cells that could last longer than several days in these environments.  We have solved this problem at Yale by designing and perfecting the first ever drift-dominated solar cell.  By collecting carriers through an electric field, we have created a solar cell that is very resilient in the intense radiation of outer space, theoretically capable of lasting decades.  In addition, our solar cell is inexpensive to manufacture, it is lightweight, and it is highly-efficient, making it an ideal choice for satellite power supplies.

 

Acknowledgements

 

            I would like to extend my thanks to Professor Jerry Woodall for allowing me to work on this project with his group.  One of his graduate students, Yanning Sun, showed me how to take all the measurements and she also provided me with past data that was very useful in creating this report.  I would also like to thank Professor Janet Pan for allowing me to perform all the necessary measurements in her laboratory.