Publication Date:
2019-07-13
Description:
Mars sample return is a major scientific goal of the 2011 US National Research Council Decadal Survey for Planetary Science. Toward achievement of this goal, recent architecture studies have focused on several mission concept options for the 2018/2020 Mars launch opportunities. Mars orbiters play multiple roles in these architectures such as: relay, landing site identification/selection/certification, collection of on-going or new measurements to fill knowledge gaps, and in-orbit collection and transportation of samples from Mars to Earth. This paper reviews orbiter concepts that combine these roles and describes a novel family of relay orbits optimized for surface operations support. Additionally, these roles provide an intersection of objectives for long term NASA science, human exploration, technology development and international collaboration.
Keywords:
Space Communications, Spacecraft Communications, Command and Tracking; Lunar and Planetary Science and Exploration; Astrodynamics
Type:
International Symposium on Space Flight Dynamics (ISSFD); Oct 29, 2012 - Nov 02, 2012; Pasadena, CA; United States
Format:
text
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