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Guide : Mrs. J. A. Thakare
About SOLAR POWER
 Renewable source
 Unlimited supply

 Efficiency
 Cost
 Need

 Benefits
 Etc..
Introduction of SPS
 The new millennium has introduced increased

pressure for finding new renewable energy sources
building a power station in space to transmit electricity
to Earth by way of radio waves-the Solar Power
Satellites.
 Microwave Wireless Power Transmission
 SPS is a clean, large-scale
 Stable electric power source
WHY SPS
 Increasing global energy demand
 Limitation of renewable energy sources

 Environmental problems due to fossil fuels.
 Overcome day & night effect and other factors such as

clouds.
 Overcome energy crisis.
SPS-THE BACKGROUND
 Peter Glaser invented the concept of a large SPS.
 The U.S Department of Energy (DOE) and the

National Aeronautics and Space Administration
(NASA) examined the SPS concept extensively
during the late 1970s.
 The central feature of this concept was the creation of a
large scale power infrastructure in space, consisting of
about 60 SPS, delivering a total of about 300GW.But, as a
result of the huge price tag, lack of evolutionary concept
and the subsiding energy crisis in 1980-1981
SPS- A GENERAL IDEA
 It is located in the geosynchronous orbit.
 Comparison between ordinary satellite.
 Comparison between terrestrial station
 Its operation.

 About structure.
SPS-MICROWAVE TRANSMISSION

 The conversion of direct power to microwave power

 The formation and control of microwave beam
 The collection of the microwave energy and its

conversion into electrical energy at the earthâ„¢s
surface.
 The key microwave components in a WPT system are
the transmitter, beam control and the receiving
antenna called RECTENNA
TRANSMITTER
 The key requirement of a transmitter is its ability to

convert dc power to RF power efficiently and radiate
the power to a controlled manner with low loss.
 The transmitterâ„¢s efficiency drives the end-to-end
efficiency as well as thermal management system.
 The main components of a transmitter include dc-toRF converter and transmitting antenna.
 The main dc-RF converters are klystrons
KLYSTRON TRASMITTER
 The tube body and

solenoid operate at
300°C and the
collector operates
at 500°C.
 The overall

efficiency is 83%.
BEAM CONTROL
 A key system and safety aspect of WPT in its ability to

control the power beam.
 Retro directive beam control systems have been the
preferred method of achieving accurate beam
pointing.
 A coded pilot signal is emitted from the rectenna
towards the SPS transmitter to provide a phase
reference for forming and pointing the power beams
POWER BEAMING FROM SPACE TO EARTH
 The efficiency for power transmission through free-space

has been shown to approach 100% and its depends on
various factors

Rt = Radius of transmitting antenna
Rr = Radius of receiving antenna
Z = distance
λ = wavelength
RECTENNA


(a) Brown’s Rectenna



(b) Brown’s Thin-Film
Rectenna



(c) Hokkaido University’s
Rectenna



(d) Kyoto University’s
Rectenna



(e) Texas A&M University’s



(f) CRL’s Rectenna



(g) Denso’s Rectenna



(h) University of Colorado’s
Rectenna
RECTENNA
 RECTENNA is the microwave to dc converting device .
 It is mainly composed of a receiving antenna and a

rectifying circuit.
 Fig. shows schematic of RECTENNA. It consists of a
receiving antenna, an input low pass filter, a rectifying
circuit and an output smoothing filter.
 In RECTENNA arrays, the diode is the most critical
component to achieve higher efficiencies because it is
the main source of loss.
LAUNCHING SYSTEM INTO SPACE


Launching the SBSP constellation into orbit is one of the most difficult
aspects of the program. Launch vehicles are expensive, operationally difficult to
use, and provide a harsh environment for the health of transported satellites
during launch. Some aspects of this architecture, however, help to mitigate
these problems:

A large number of small satellites can fit into a single launch vehicle.
Modularity of the system means scope can be expanded or reduced to fit
available launch vehicle payload capabilities.

The overall efficiency of this distributed satellite array of collectors,
beamers and sub-beamers is 49%, but the overall return on investment is much
higher as modularity allows one to put in a large swarm of low-cost satellites in
orbit to generate a higher power output. Given recent advances in microwave
beaming and DC to microwave conversion and vice versa at high efficiency
rates, falling launch cost for satellites, and the operational robustness of the
distributed architecture of solar power satellites proposed here, the time has
come to phase out our dependence on fossil fuels and incorporate SBSP power
into Earth’s electrical grids.
ADVANTAGES
 The power could be directed to any point on the earth







surface.
The power density would be uninterrupted by
darkness, clouds, or precipitation, which are the
problems encountered with earth based solar arrays.
The realization of the SPS concept holds great
promises for solving energy crisis
No moving parts.
No fuel required.
No waste product.
DISADVANTAGES
 The main draw back of solar energy transfer from orbit is the







storage of electricity during off peak demand hours.
The frequency of beamed radiation is planned to be at 2.45 GHz
and this frequency is used by communication satellites also.
The entire structure is massive.
High cost and require much time for construction.
Radiation hazards associated with the system.
Risks involved with malfunction.
High power microwave source and high gain antenna can be
used to deliver an intense burst of energy to a target and thus
used as a weapon
CONCLUSION


The SPS will be a central attraction of space and energy
technology in coming decades. However, large scale retro directive
power transmission has not yet been proven and needs further
development. Another important area of technological development
will be the reduction of the size and weight of individual elements in
the space section of SPS. Large-scale transportation and robotics for
the construction of large-scale structures in space include the other
major fields of technologies requiring further developments. Technical
hurdles will be removed in the coming one or two decades. Finally, we
look forward to universal acceptance of the premise the
electromagnetic energy is a tool to improve the quality of life for
mankind. It is not a pollutant but more aptly, a man made extension of
the naturally generated electromagnetic spectrum that provides heat
and light for our sustenance. From this view point, the SPS is merely a
down frequency converter from the visible spectrum to microwaves.
Solar pwer satellite

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Solar pwer satellite

  • 1. Guide : Mrs. J. A. Thakare
  • 2. About SOLAR POWER  Renewable source  Unlimited supply  Efficiency  Cost  Need  Benefits  Etc..
  • 3. Introduction of SPS  The new millennium has introduced increased pressure for finding new renewable energy sources building a power station in space to transmit electricity to Earth by way of radio waves-the Solar Power Satellites.  Microwave Wireless Power Transmission  SPS is a clean, large-scale  Stable electric power source
  • 4. WHY SPS  Increasing global energy demand  Limitation of renewable energy sources  Environmental problems due to fossil fuels.  Overcome day & night effect and other factors such as clouds.  Overcome energy crisis.
  • 5. SPS-THE BACKGROUND  Peter Glaser invented the concept of a large SPS.  The U.S Department of Energy (DOE) and the National Aeronautics and Space Administration (NASA) examined the SPS concept extensively during the late 1970s.  The central feature of this concept was the creation of a large scale power infrastructure in space, consisting of about 60 SPS, delivering a total of about 300GW.But, as a result of the huge price tag, lack of evolutionary concept and the subsiding energy crisis in 1980-1981
  • 6. SPS- A GENERAL IDEA  It is located in the geosynchronous orbit.  Comparison between ordinary satellite.  Comparison between terrestrial station  Its operation.  About structure.
  • 7.
  • 8. SPS-MICROWAVE TRANSMISSION  The conversion of direct power to microwave power  The formation and control of microwave beam  The collection of the microwave energy and its conversion into electrical energy at the earthâ„¢s surface.  The key microwave components in a WPT system are the transmitter, beam control and the receiving antenna called RECTENNA
  • 9.
  • 10.
  • 11. TRANSMITTER  The key requirement of a transmitter is its ability to convert dc power to RF power efficiently and radiate the power to a controlled manner with low loss.  The transmitterâ„¢s efficiency drives the end-to-end efficiency as well as thermal management system.  The main components of a transmitter include dc-toRF converter and transmitting antenna.  The main dc-RF converters are klystrons
  • 12. KLYSTRON TRASMITTER  The tube body and solenoid operate at 300°C and the collector operates at 500°C.  The overall efficiency is 83%.
  • 13. BEAM CONTROL  A key system and safety aspect of WPT in its ability to control the power beam.  Retro directive beam control systems have been the preferred method of achieving accurate beam pointing.  A coded pilot signal is emitted from the rectenna towards the SPS transmitter to provide a phase reference for forming and pointing the power beams
  • 14. POWER BEAMING FROM SPACE TO EARTH  The efficiency for power transmission through free-space has been shown to approach 100% and its depends on various factors Rt = Radius of transmitting antenna Rr = Radius of receiving antenna Z = distance λ = wavelength
  • 15. RECTENNA  (a) Brown’s Rectenna  (b) Brown’s Thin-Film Rectenna  (c) Hokkaido University’s Rectenna  (d) Kyoto University’s Rectenna  (e) Texas A&M University’s  (f) CRL’s Rectenna  (g) Denso’s Rectenna  (h) University of Colorado’s Rectenna
  • 16. RECTENNA  RECTENNA is the microwave to dc converting device .  It is mainly composed of a receiving antenna and a rectifying circuit.  Fig. shows schematic of RECTENNA. It consists of a receiving antenna, an input low pass filter, a rectifying circuit and an output smoothing filter.  In RECTENNA arrays, the diode is the most critical component to achieve higher efficiencies because it is the main source of loss.
  • 17. LAUNCHING SYSTEM INTO SPACE  Launching the SBSP constellation into orbit is one of the most difficult aspects of the program. Launch vehicles are expensive, operationally difficult to use, and provide a harsh environment for the health of transported satellites during launch. Some aspects of this architecture, however, help to mitigate these problems:  A large number of small satellites can fit into a single launch vehicle. Modularity of the system means scope can be expanded or reduced to fit available launch vehicle payload capabilities.  The overall efficiency of this distributed satellite array of collectors, beamers and sub-beamers is 49%, but the overall return on investment is much higher as modularity allows one to put in a large swarm of low-cost satellites in orbit to generate a higher power output. Given recent advances in microwave beaming and DC to microwave conversion and vice versa at high efficiency rates, falling launch cost for satellites, and the operational robustness of the distributed architecture of solar power satellites proposed here, the time has come to phase out our dependence on fossil fuels and incorporate SBSP power into Earth’s electrical grids.
  • 18. ADVANTAGES  The power could be directed to any point on the earth      surface. The power density would be uninterrupted by darkness, clouds, or precipitation, which are the problems encountered with earth based solar arrays. The realization of the SPS concept holds great promises for solving energy crisis No moving parts. No fuel required. No waste product.
  • 19. DISADVANTAGES  The main draw back of solar energy transfer from orbit is the       storage of electricity during off peak demand hours. The frequency of beamed radiation is planned to be at 2.45 GHz and this frequency is used by communication satellites also. The entire structure is massive. High cost and require much time for construction. Radiation hazards associated with the system. Risks involved with malfunction. High power microwave source and high gain antenna can be used to deliver an intense burst of energy to a target and thus used as a weapon
  • 20. CONCLUSION  The SPS will be a central attraction of space and energy technology in coming decades. However, large scale retro directive power transmission has not yet been proven and needs further development. Another important area of technological development will be the reduction of the size and weight of individual elements in the space section of SPS. Large-scale transportation and robotics for the construction of large-scale structures in space include the other major fields of technologies requiring further developments. Technical hurdles will be removed in the coming one or two decades. Finally, we look forward to universal acceptance of the premise the electromagnetic energy is a tool to improve the quality of life for mankind. It is not a pollutant but more aptly, a man made extension of the naturally generated electromagnetic spectrum that provides heat and light for our sustenance. From this view point, the SPS is merely a down frequency converter from the visible spectrum to microwaves.