Third generation commercial solar electric propulsion: A foundation for space exploration missions

Solar Electric Propulsion (SEP) has become vital in several commercial space applications and is well positioned to lower the cost and risk of important space exploration and science missions. The success of commercial SEP in the global satellite market provides a production base that produces cost-effective hardware. Well-established commercial approaches are in place for scaling and tailoring SEP systems to US government missions. An evolutionary roadmap is discussed, illustrating how these capabilities have emerged from the privately funded commercial technology branching into two new applications to government exploration missions. One is the adaptation for deep space exploration as illustrated by the NASA Discovery class mission to the main belt asteroid 16 Psyche that will use currently-available commercial SEP technologies with only minor modifications. The second enables the emergence of large scale space transportation as embodied by the Power Propulsion Element (PPE), derived from the Asteroid Redirect Robotic Mission (ARRM) spacecraft concept and planned as the bus foundation of the Deep Space Gateway (DSG). The PPE could use high-power third generation SEP derived from commercial capabilities to transport and maintain large habitats and modules within the Earth-Moon system.

[1]  Danielle Marsh,et al.  Overview of the spacecraft design for the Psyche mission concept , 2018, 2018 IEEE Aerospace Conference.

[2]  John Baker,et al.  Human Missions to Mars Orbit, Phobos, and Mars Surface Using 100-kWe-Class Solar Electric Propulsion , 2014 .

[3]  Charles E. Garner,et al.  Low-Power Operation and Plasma Characterization of a Qualification Model SPT-140 Hall Thruster , 2015 .

[4]  Dan M. Goebel,et al.  Solar Electric Propulsion for Discovery-Class Missions , 2014 .

[5]  John Steven Snyder,et al.  Throttled Performance of the SPT-140 Hall Thruster , 2014 .

[6]  James H. Gilland,et al.  Performance, Facility Pressure Effects, and Stability Characterization Tests of NASA's Hall Effect Rocket with Magnetic Shielding Thruster , 2016 .

[7]  Timothy R. Sarver-Verhey,et al.  The 12.5 kW Hall Effect Rocket with Magnetic Shielding (HERMeS) for the Asteroid Redirect Robotic Mission , 2016 .

[8]  Peter Lord,et al.  Adaptability of the SSL SPT-140 Subsystem for use on a NASA Discovery Class Missions: Psyche , 2016 .

[9]  G. G. Stokes "J." , 1890, The New Yale Book of Quotations.

[10]  I. Mikellides,et al.  Design of a Laboratory Hall Thruster with Magnetically Shielded Channel Walls, Phase I: Numerical Simulations , 2011 .

[11]  Andrew E. Turner,et al.  Establishing Affordable Mars Telecom Relay Service , 2016 .

[12]  I. Mikellides,et al.  Design of a Laboratory Hall Thruster with Magnetically Shielded Channel Walls, Phase II: Experiments , 2012 .

[13]  I. Katz,et al.  Fundamentals of Electric Propulsion: Ion and Hall Thrusters , 2008 .