Solar panels on spacecraft
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current uses -- see talk page
{{Unreferenced|date=November 2006}}
{{Merge| Space solar power | Talk:Space solar power#Merge|date=February 2008}}
Spacecraft operating in the inner [[solar system]] usually rely on the use of [[photovoltaic]] [[Photovoltaic module|solar panel]]s to derive electricity from [[sunlight]]. In the outer solar system, where the sunlight is too weak to produce sufficient power, [[radioisotope thermal generator]]s (RTGs) are used as a power source<ref name="EPSD">NASA JPL Publication: Basics of Space Flight, Chapter 11. Typical Onboard Systems , Electrical Power Supply and Distribution Subsystems, http://www2.jpl.nasa.gov/basics/bsf11-3.html</ref>.
==History==
The first spacecraft to use solar panels was the [[Vanguard 1]] satellite, launched by the US in 1958.
This was largely because of the influence of Dr.[[Hans Ziegler]], who can be regarded as the father of spacecraft solar power. <ref>{{cite web
| last =Perlin
| first =John
| authorlink =
| coauthors =
| title =Late 1950s - Saved by the Space Race
| work =SOLAR EVOLUTION - The History of Solar Energy
| publisher =The Rahus Institute
| date =Pub date unknown
| url =http://www.californiasolarcenter.org/history_pv.html
| format =HTML
| doi =
| accessdate =2007-02-25 }}</ref>. Of his 30 year tenure at [[Fort Monmouth]] (1947-1976), Ziegler spent 12 years in the top position as Chief Scientist<ref>[http://www.ieee.org/web/aboutus/history_center/publications/sources1/archival_collectionsz.html IEEE Archival Collection]</ref>.
== Uses ==
Solar panels on spacecraft supply power for 2 main uses:
* power to run the sensors, active heating and cooling, and telemetry.
* power for [[spacecraft propulsion]] -- [[electric propulsion]], sometimes called solar-electric propulsion<ref name="NASA11">NASA JPL Publication: Basics of Space Flight, Chapter 11. Typical Onboard Systems, Propulsion Subsystems, http://www2.jpl.nasa.gov/basics/bsf11-4.html#propulsion</ref>. See also [[Tsiolkovsky rocket equation#energy|energy needed for propulsion methods]].
For both uses, the [[figure of merit]] of the solar panels (and RTGs) is the power generated per kg, as an upper limit of the power the spacecraft has at its disposal per kg spacecraft (including solar panels).
To increase the power generated per kg, typical solar panels on spacecraft use close-packed solar cell rectangles that cover nearly 100% of the sun-visible area of the solar panels,
rather than the [[solar wafer]] circles which, even though close-packed, [[Sphere_packing#Circle_packing | cover about 90%]] of the sun-visible area of typical solar panels on earth.
However, some solar panels on spacecraft have solar cells that cover only 30% of the sun-visible area<ref name="NASA11" />.
==Implementation==
Solar panels need to have a lot of surface area that can be pointed towards the Sun as the spacecraft moves. More exposed surface area means more electricity can be converted from light energy from the Sun. Since spacecraft have to be small, this limits the amount of power that can be produced <ref name="EPSD"/>.
Spacecraft are built so that the solar panels can be pivoted as the spacecraft moves. Thus, they can always stay in the direct path of the light rays no matter how the spacecraft is pointed. Spacecraft are usually designed with solar panels that can always be pointed at the Sun, even as the rest of the body of the spacecraft moves around, much as a tank turret can be aimed independently of where the tank is going. A tracking mechanism is often incorporated into the solar arrays to keep the array pointed towards the sun<ref name="EPSD"/>.
Sometimes, satellite operators purposefully orient the solar panels to "off point," or out of direct alignment from the Sun. This happens if the batteries are completely charged and the amount of electricity needed is lower than the amount of electricity made; off-pointing is also sometimes used on the International Space Station for orbital [[Night Glider mode|drag reduction]].
==Types of solar cells typically used==
[[Gallium arsenide]]-based solar cells are typically favored over silicon in industry, because they have a higher efficiency. The most efficient solar cells currently in production are multi-junction cells. These use a combination of several layers of both gallium arsenide and silicon to capture the largest spectrum of light possible. Leading edge multi-junction cells are capable of nearly 29% efficiency under ideal conditions. <ref>[http://ieeexplore.ieee.org/iel3/4263/12206/00564003.pdf?arnumber=564003.pdf Cost Performance of Multi-Junction, Gallium Arsenide, and Silicon Solar Cells on Spacecraft.]</ref>
==Spacecraft that have used solar power==
To date, solar power, other than for propulsion, has been practical for spacecraft operating no farther from the [[sun]] than the orbit of [[Mars (planet)|Mars]]. For example, [[Magellan probe|Magellan]], [[Mars Global Surveyor]], and [[Mars Observer]] used solar power as does the Earth-orbiting, [[Hubble Space Telescope]]. The [[Rosetta space probe]], launched [[March 2]], [[2004]], will use solar panels as far as the orbit of [[Jupiter]] (5.25 [[Astronomical unit|AU]]); previously the furthest use was the [[Stardust (spacecraft)|Stardust spacecraft]] at 2 AU. Solar power for propulsion was also used on the European lunar mission [[SMART-1]] with a [[Hall effect thruster]].
The upcoming ''[[Juno (space mission)|Juno]]'' mission will be the first mission to Jupiter to use solar panels instead of the traditional RTGs that are used by previous outer solar system missions<ref>[http://newfrontiers.nasa.gov/missions_juno.html Juno mission page at NASA's New Frontiers Web Site]. Retrieved [[2007]]-[[August 31|08-31]].</ref>.
==Power Available==
In 2005 Rigid-Panel Stretched Lens Arrays were producing 7 kW per wing. Solar arrays producing 300 W/kg and 300 W/m² from the sun's 1366 W/m² energy near the Earth are available. Entech Inc. hopes to develop 100 kW panels by 2010 and 1 MW panels by 2015.
<ref>[http://www.entechsolar.com/SPRAT05b.pdf Paper. Stretched Lens Array SquareRigger
(SLASR) Technology Maturation by Mark O’Neill et all]</ref>
==Future Uses==
For future missions, it is desirable to reduce solar array mass, and to increase the power generated per unit area. This will reduce overall spacecraft mass, and may make the operation of solar-powered spacecraft feasible at larger distances from the sun. Solar array mass could be reduced with thin-film photovoltaic cells, flexible blanket substrates, and composite support structures. Solar array efficiency could be improved by using new photovoltaic cell materials and solar concentrators that intensify the incident sunlight. Photovoltaic concentrator solar arrays for primary spacecraft power are devices which intensify the sunlight on the photovoltaics. This design uses a flat lens, called a [[Fresnel lens]], which takes a large area of sunlight and concentrates it onto a smaller spot. The same principle is used to start fires with a [[magnifying glass]] on a sunny day.
Solar concentrators put one of these lenses over every solar cell. This focuses light from the large concentrator area down to the smaller cell area. This allows the quantity of expensive solar cells to be reduced by the amount of concentration. Concentrators work best when there is a single source of light and the concentrator can be pointed right at it. This is ideal in space, where the Sun is a single light source. Solar cells are the most expensive part of solar arrays, and arrays are often a very expensive part of the spacecraft. This technology may allow costs to be cut significantly due to the utilization of less material.
It has been proposed that it may be possible to develop space-based solar plants — [[solar power satellite]]s with large arrays of photovoltaic cells-- that would beam the energy they produce to Earth using [[microwave power transmission|microwaves]] or lasers. This could, in principle, be a significant source of electrical power generated using non-fossil fuel sources. Japanese and [[ESA|European space agencies]], among others, are analyzing the possibility of developing such power plants in the 21st century.
==See also==
*Main article on [[space solar power]]
*Main article on [[solar cells]]
*Main article on [[Photovoltaic array]]s
*For solar arrays on the [[International Space Station]], see [[ISS_Solar_Arrays#Solar_arrays]] or [[Electrical system of the International Space Station]]
==References==
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<references/>
[[Category:Spacecraft components]]
[[Category:Extra terrestrial photovoltaics]]