The Heliopause Electrostatic Rapid Transit System (HERTS) - Design, Trades, and Analyses Performed in a Two Year NASA Investigation of Electric Sail Propulsion Systems
Author(s) -
Bruce M. Wiegmann
Publication year - 2017
Publication title -
53rd aiaa/sae/asee joint propulsion conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2017-4712
Subject(s) - propulsion , aerospace engineering , electrically powered spacecraft propulsion , transit (satellite) , aeronautics , ion thruster , engineering , environmental science , transport engineering , public transport
known as the Electric Sail (E-Sail) for future scientific exploration missions. This team initially won a NASA Space Technology Mission Directorate (STMD) Phase I NASA Innovative Advanced Concept (NIAC) award and then a two-year follow-on Phase II NIAC award in October 2015. This paper documents the findings from this three-year investigation. An Electric sail, a propellant-less propulsion system, uses solar wind ions to rapidly travel either to deep space or the inner solar system. Scientific spacecraft could reach Pluto in ~5 years, or the boundary of the solar system in ten to twelve years compared to the thirty-five plus years the Voyager spacecraft took. The team’s recent focuses have been: 1) Developing a Particle in Cell (PIC) numeric engineering model from MSFC’s experimental data on the interaction between simulated solar wind and a charged bare wire that can be applied to a variety of missions, 2) Determining what missions could benefit from this revolutionary propulsion system, 3) Conceptualizing spacecraft designs for various tasks: to reach the solar system’s edge, to orbit the sun as Heliophysics sentinels, or to examine a multitude of asteroids.
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