Data for: A Satellite Mission Concept for High Drag Environments
Published: 18 July 2019| Version 1 | DOI: 10.17632/w8dt6bc7ff.1
Contributor:
Lance McCrearyDescription
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.
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Categories
Systems Engineering, Space Mission, System Architecture, Space Engineering, Advanced Space Propulsion