Mars Mission Applications Enabled By A High-Power Solar Electric Propulsion (SEP) Power and Propulsion Element (PPE)With the culmination of years of research and development in space solar power and electric propulsion systems, NASA and its partner Lanteris (formerly Maxar) are designing and building a high-power SEP Stage called the Power and Propulsion Element (PPE). High power Solar Electric Propulsion (SEP) systems can enable a wide range of exploration missions, both human and robotic. In its specific application, the PPE is being designed to provide power and propulsion for Gateway, an orbital platform that will support long-term exploration missions on the moon’s surface, as part of NASA’s Artemis program. The PPE itself is a technology development effort, meant to both support the lunar exploration missions, and enable future missions through high power SEP. This paper will examine the applicability of a high power SEP system similar to the PPE’s specifications to a series of Mars mission concepts designed by NASA Glenn’s Concurrent Engineering Compass team, including its usage as both a spacecraft and a payload delivery vehicle.
Document ID
20250011002
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Melissa L McGuire (Glenn Research Center Cleveland, United States)
David A Smith (HX5 (United States) Fort Walton Beach, Florida, United States)
Maya N Havens (Glenn Research Center Cleveland, United States)
Steven R Oleson (Glenn Research Center Cleveland, United States)
Elizabeth R Turnbull (Glenn Research Center Cleveland, United States)
Date Acquired
December 3, 2025
Subject Category
Spacecraft Propulsion and PowerSpacecraft Design, Testing and PerformanceAstrophysics
Meeting Information
Meeting: SciTech Forum
Location: Orlando, FL
Country: US
Start Date: January 12, 2026
End Date: January 16, 2026
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 837933.02.12.03
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
low thrust propulsiontrajectory designmars explorationspacecraft designsolar electric propulsionelectric propulsion