Data for: A Satellite Mission Concept for High Drag Environments

Published: 18 Jul 2019 | Version 1 | DOI: 10.17632/w8dt6bc7ff.1
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Description of this data

This manuscript follows an established and robust Systems Engineering process to propose a space mission concept that uses in-situ Low Earth Orbit resources, comprised mostly of N, O, N2, and O2, as propellant.

Experiment data files

This data is associated with the following publication:

A satellite mission concept for high drag environments

Published in: Aerospace Science and Technology

Latest version

  • Version 1

    2019-07-18

    Published: 2019-07-18

    DOI: 10.17632/w8dt6bc7ff.1

    Cite this dataset

    McCreary, Lance (2019), “Data for: A Satellite Mission Concept for High Drag Environments”, Mendeley Data, v1 http://dx.doi.org/10.17632/w8dt6bc7ff.1

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Categories

Systems Engineering, Space Mission, System Architecture, Space Engineering, Advanced Space Propulsion

Licence

CC BY 4.0 Learn more

The files associated with this dataset are licensed under a Creative Commons Attribution 4.0 International licence.

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