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  2. Roll Out Solar Array - Wikipedia

    en.wikipedia.org/wiki/Roll_Out_Solar_Array

    Traditional solar panels used to power satellites are bulky, with heavy panels folded together using mechanical hinges. Given a space-bound payload is limited in its mass and volume by necessity, ROSA is 20 percent lighter (with a mass of 325 kg (717 lb)) [ 3 ] and one-fourth the volume of rigid panel arrays with the same performance.

  3. Opportunity (rover) - Wikipedia

    en.wikipedia.org/wiki/Opportunity_(rover)

    At the start of the mission the solar panels could provide up to around 900 watt-hours (Wh) per day to recharge the battery and power system in one Sol, but this could vary due to a variety of factors. [48] In Eagle crater the cells were producing about 840 Wh per day, but by Sol 319 in December 2004, it had dropped to 730 Wh per day. [50]

  4. Solar panels on spacecraft - Wikipedia

    en.wikipedia.org/wiki/Solar_panels_on_spacecraft

    To increase the specific power, 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, cover about 90% of the Sun-visible area of typical solar panels on Earth. However, some solar panels on ...

  5. Intuitive Machines Nova-C - Wikipedia

    en.wikipedia.org/wiki/Intuitive_Machines_Nova-C

    Nova-C landers use solar panels as a source of electrical power. Most areas of the lunar surface are sunlit during lunar days , which last approximately fourteen Earth days. Electrical power is generated by a photovoltaic system with three solar panels, a top deck panel and two body panels, generating a combined maximum of 200 W on the lunar ...

  6. Solar electric propulsion - Wikipedia

    en.wikipedia.org/wiki/Solar_electric_propulsion

    In particular the high specific impulse of the ion engines could lower overall mass and avoid having to use nuclear technology for power when coupled with solar panels. [2] A 1998 study for SEP for a human mission suggest that a human-sized spacecraft would need 600 to 800 kilowatts of electrical power coupled with ion engines with a specific ...

  7. Rosetta (spacecraft) - Wikipedia

    en.wikipedia.org/wiki/Rosetta_(spacecraft)

    Electrical power for the spacecraft came from two solar arrays totalling 64 square metres (690 sq ft). [54] Each solar array was subdivided into five solar panels, with each panel being 2.25 × 2.736 m (7.38 × 8.98 ft). The individual solar cells were made of silicon, 200 μm thick, and 61.95 × 37.75 mm (2.44 × 1.49 in). [55]