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  2. Space-based solar power - Wikipedia

    en.wikipedia.org/wiki/Space-based_solar_power

    Orbiting satellites can be exposed to a consistently high degree of solar radiation, generally for 24 hours per day, whereas earth surface solar panels currently collect power for an average of 29% of the day.

  3. Solar panels on spacecraft - Wikipedia

    en.wikipedia.org/wiki/Solar_panels_on_spacecraft

    For example, Juno, Magellan, Mars Global Surveyor, and Mars Observer used solar power as does the Earth-orbiting, Hubble Space Telescope. The Rosetta space probe, launched 2 March 2004, used its 64 square metres (690 sq ft) of solar panels [15] as far as the orbit of Jupiter (5.25 AU); previously the furthest use was the Stardust spacecraft at 2

  4. Electrical system of the International Space Station - Wikipedia

    en.wikipedia.org/wiki/Electrical_system_of_the...

    International Space Station solar array wing (Expedition 17 crew, August 2008).An ISS solar panel intersecting Earth's horizon.. The electrical system of the International Space Station is a critical part of the International Space Station (ISS) as it allows the operation of essential life-support systems, safe operation of the station, operation of science equipment, as well as improving crew ...

  5. California gives green light to space-based solar power project

    www.aol.com/news/2009-12-04-california-gives...

    The Southern California start-up is developing technology for what it hopes will be an orbiting solar power collection system that could add a whopping 200 megawatts to the Golden State's ...

  6. Vanguard 1 - Wikipedia

    en.wikipedia.org/wiki/Vanguard_1

    Vanguard 1 (Harvard designation: 1958-Beta 2, [3] COSPAR ID: 1958-002B [1]) is an American satellite that was the fourth artificial Earth-orbiting satellite to be successfully launched, following Sputnik 1, Sputnik 2, and Explorer 1. It was launched 17 March 1958. Vanguard 1 was the first satellite to have solar electric power. [4]

  7. International Space Station - Wikipedia

    en.wikipedia.org/wiki/International_Space_Station

    Power is stabilised and distributed at 160 V DC and converted to the user-required 124 V DC. The higher distribution voltage allows smaller, lighter conductors, at the expense of crew safety. The two station segments share power with converters. The USOS solar arrays are arranged as four wing pairs, for a total production of 75 to 90 kilowatts. [3]

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