Term "CubeSat" was coined to denote nanosatellites that adhere to the standards described in the CubeSat design specification.
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Term "CubeSat" was coined to denote nanosatellites that adhere to the standards described in the CubeSat design specification.
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CubeSat structures do not have all the same strength concerns as larger satellites do, as they have the added benefit of the deployer supporting them structurally during launch.
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CubeSat computers are highly susceptible to radiation and builders will take special steps to ensure proper operation in the high radiation of space, such as the use of ECC RAM.
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CubeSat propulsion has made rapid advancements in the following technologies: cold gas, chemical propulsion, electric propulsion, and solar sails.
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The biggest challenge with CubeSat propulsion is preventing risk to the launch vehicle and its primary payload while still providing significant capability.
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Electric propulsion systems are disadvantaged in their use of power, which requires the CubeSat to have larger solar cells, more complicated power distribution, and often larger batteries.
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One of the earliest CubeSat launches was on 30 June 2003 from Plesetsk, Russia, with Eurockot Launch Services's Multiple Orbit Mission.
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Miniature X-ray Solar Spectrometer CubeSat is a 3U launched to the International Space Station on 6 December 2015 from where it was deployed on 16 May 2016.
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The mission CubeSat technology is called Mars Cube One, each one is a six-unit CubeSat, 14.
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Some CubeSat deployers are created by companies, such as the ISIPOD or SPL, while some have been created by governments or other non-profit institutions such as the X-POD, T-POD, or the J-SSOD on the International Space Station.
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