Data for: A Satellite Mission Concept for High Drag Environments

Published: 18 Jul 2019 | Version 1 | DOI: 10.17632/w8dt6bc7ff.1

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


    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


Views: 59
Downloads: 7


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


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