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Space-based solar power (SSP) generation is being touted as a solution to our ever-increasing energy consumption and dependence on fossil fuels. Satellites in Earth's orbit can capture solar energy through photovoltaic cells and transmit that power to ground based stations. Solar cells in orbit are not hindered by weather, clouds, or night. The energy generated by this process is clean and pollution-free. Although the concept of space-based solar power was initially proposed nearly 40 years ago, the level of technology in photovoltaics, power transmission, materials, and efficient satellite design has finally reached a level of maturity that makes solar power from space a feasible prospect.
Furthermore, new strategies in methods for solar energy acquisition and transmission can lead to simplifications in
design, reductions in cost and reduced risk.
This paper proposes using a distributed array of small satellites to collect power from the Sun, as compared to the more
traditional SSP design that consists of one monolithic satellite. This concept mitigates some of SSP's most troublesome
historic constraints, such as the requirement for heavy lift launch vehicles and the need for significant assembly in space.
Instead, a larger number of smaller satellites designed to collect solar energy are launched independently. A high
frequency beam will be used to aggregate collected power into a series of transmission antennas, which beam the energy
to Earth's surface at a lower frequency. Due to the smaller power expectations of each satellite and the relatively short
distance of travel from low earth orbit, such satellites can be designed with smaller arrays. The inter-satellite rectenna
devices can also be smaller and lighter in weight.
Our paper suggests how SSP satellites can be designed small enough to fit within ESPA standards and therefore use
rideshare to achieve orbit. Alternatively, larger versions could be launched on Falcon 9s or on Falcon 1s with booster
stages. The only satellites that are constrained to a significant mass are the beam-down satellites, which still require
significant transmission arrays to sufficiently focus the beams targeting corresponding ground stations. With robust
design and inherent redundancy built-in, power generation and transmission will not be interrupted in the event of
mishaps like space debris collision. Furthermore, the "plug and play" nature of this system significantly reduces the
cost, complexity, and risk of upgrading the system. The distributed nature of smallsat clusters maximizes the use of
economies of scale.
This approach retains some problems of older designs and introduces additional ones. Mitigations will be explored
further. For example, the distributed nature of the system requires very precise coordination between and among
satellites and a mature attitude control and determination system. Such a design incorporates multiple beaming stages,
which has the potential to reduce overall system efficiency. Although this design eliminates the need for space
assembly, it retains the challenge of significant on-orbit deployment of solar and transmission arrays.
Space power "beaming" is a three step process that involves: 1) conversion of dc power generated by solar cells on the
satellite into an electromagnetic wave of suitable frequency, 2) transmission of that wave to power stations on ground, and 3) conversion of the radio waves back into dc power. A great deal of research has been done on the use of microwaves for this purpose. Various factors that affect efficient power generation and transmission will be analyzed in this paper. Based on relevant theory and performance and optimization models, the paper proposes solutions that will help make space-based solar power generation a practical and viable option for addressing the world's growing energy needs.
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