Space Solar Power Station/Satellite (SPS)
The concept
of the SPS is very simple. It is a gigantic
satellite designed as an electric power plant orbiting in the Geostationary
Earth Orbit (GEO). It consists of mainly three segments; solar energy collector
to convert the solar energy into DC (direct current) electricity,
In 2009 in
Japan, ‘Basic Plan for Space Policy’ was published, on which ‘As a program that corresponds to the following major social needs and
goals for the next 10 years, a Space Solar Power Program will be targeted for
the promotion of the 5-year development and utilization plan.’ We need both
technical advance and ‘surprise’ in the next space experiment based on the Basic
Plan for Space Policy.
The SPS
system has advantage in producing electricity with much higher efficiency
compared with a photovoltaic system on the ground. Since SPS is placed in space
such as the GEO there is no atmospheric absorption, the solar input power is
about 30% higher density compared with the ground solar power density, and is
available 24 hours (except for 70 minutes maximum during 42 days near the
equinoxes as without affected by the weather condition. Solar flux is
approximately 8 times higher in space than the long-term surface average on the
ground if the insolation is 4 kWh/m2/day. For the terrestrial
system, however, the efficiency, additional space due to the loss, and cost of
the storage system should be taken into consideration in order to supply
electricity 24 hours. This ratio would become higher depend on the efficiency
since the 100 % efficiency is assumed in the storage system. The possible
issues to be discussed on the SPS system are the microwave power beam impact on
the existing communication networks and bio-bodies.
A huge and
clean power source is to be developed for sustainable economic activities with
a sufficient suppression of CO2 emission. Only solar technologies
can provide a huge and clean power source in the near future. The terrestrial
photovoltaics, wind, geothermal, and other natural resources depend on the
environmental conditions and are neither stable nor sufficient.
In the
over-all SPS System, the output of the photovoltaic cell panel is converted to
microwave, transmitted to the ground rectenna system, and converted back to
DC. An aperture of a microwave
transmitting antenna array can be designed with freedom of parameters such as
the microwave operating frequency and the antenna element spacing. The dimension of the rectenna site on
the ground is dependent on the transmitting antenna size and the beam (power)
collection efficiency.
Assuming 70% conversion rate in the space segment, 90% beam (power)
collection efficiency, and 80% conversion rate in the ground segment, the
estimated over-all efficiency from DC (output of the solar panel) to DC (output
from the rectenna system) is approximately 50%.
The SPS space
segment consists of solar cells, RF circuits and antennas, a sensor for the
pilot signal, and a control unit for beam forming and retrodirectivity, and
circuit power supply. The SPS
system of 1 GW power plant has the following typical dimensions. The area of a
solar cell panel is approximately 10 km2 (2km x 5km) for production
of 2GW DC power with the solar cell conversion efficiency of 15%. For the transmitting antenna array, one
typical dimension will be 1km in diameter.
According to the request of the beam collecting efficiency, an aperture
distribution of the transmitting antenna is determined such as uniform profile
or Gaussian profile. Assuming the
antenna element spacing of 0.75λ=3.8cm at 5.8GHz, the radiator weight density
of 2.69g/cc and 160 antenna elements, one could get 9.6 kg/ m2 with this design approach.
In 2007, the IPCC (Intergovernmental Panel on Climate Change) concluded in the Fourth
Assessment Report there is no doubt that human activities have caused the
global warming. They estimate surface air warming in the 21st century)
Best estimate for a “low scenario” is 1.8 °C with a likely range of 1.1 to 2.9
°C, 2) Best estimate for a “high scenario” is 4.0 °C with a likely range of 2.4
to 6.4 °C, 3) A temperature rise of about 0.2 °C per decade is projected for
the next two decades for all scenarios. They conclude that we have to reduce
the all
long-lived greenhouse gases by 50%.
What is real cause of change of the global environment? Human activities or
Human being itself? We have to consider the cause and solve the answer of
social dilemma
between the global environment and human activities. In this paper,
we discuss a possibility of space environment use is most hopeful answer of the
social dilemma.
The SPS is best solution to reduce the CO2 emission and expand our sustainable
humanosphere to the space.