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Integration and Test

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Low Earth Orbit Satellite Design

Part of the book series: Space Technology Library ((SPTL,volume 36))

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Abstract

Integration is the process of testing the components of the spacecraft, assembling them, putting the completed spacecraft through functional testing, then performing thermal, vibration and thermal vacuum tests. After that, the spacecraft is ready to be shipped to the launch site, where it is functionally retested to ensure that no damage was done to the spacecraft. Then, the spacecraft is integrated with the launch vehicle.

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© 2018 Springer International Publishing AG

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Sebestyen, G., Fujikawa, S., Galassi, N., Chuchra, A. (2018). Integration and Test. In: Low Earth Orbit Satellite Design. Space Technology Library, vol 36. Springer, Cham. https://doi.org/10.1007/978-3-319-68315-7_14

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  • DOI: https://doi.org/10.1007/978-3-319-68315-7_14

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-68314-0

  • Online ISBN: 978-3-319-68315-7

  • eBook Packages: EngineeringEngineering (R0)

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