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High Power Advanced Solar Electric Propulsion Development Under NASA's NextSTEP ProjectHuman missions to Mars will require next generation solar electric propulsion (SEP) systems that can operate at power levels of 300 kW or higher to efficiently transport crew and cargo. In the mid-2020s, NASA is planning to launch the Deep Space Gateway (DSG), which is a crew-tended habitat that will be placed in orbit around the Moon. NASA is developing 12.5 kW Hall thrusters for the DSG. In the late 2020s, the DSG will be followed by a second vehicle, called the Deep Space Transport (DST), which will simulate a crewed Mars mission in cislunar space. In parallel with the 12.5 kW thrusters for the DSG, NASA is initiating development of 100 kW thrusters for potential demonstration on the DST. In 2016, NASA issued a Next Space Technologies for Exploration Partnerships (NextSTEP) Broad Agency Announcement to solicit proposals for development of high-power electric thrusters. The partnerships require at least 50 percent cost sharing by the companies. Three companies were selected for development activities lasting up to three years: Ad Astra, Aerojet Rocketdyne, and MSNW. Ad Astra is developing a Variable Specific Impulse Magnetoplasma Rocket (VASIMR), Aerojet Rocketdyne is developing a Nested Hall Thruster (NHT), and MSNW is developing an Electrodeless Lorentz Force (ELF) plasma thruster. The primary goal of these activities is to operate the thrusters at 100 kW for 100 continuous hours in a vacuum chamber. In addition to the thrusters, the companies are developing Power Processing Units (PPUs), propellant feed systems, and thermal management systems. This presentation will describe the three activities, the progress they have made in achieving the primary testing goal, the technical challenges they have encountered, and discuss the importance of extensibility.
Document ID
20190001010
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Moore, Chris
(NASA Headquarters Washington, DC United States)
Pencil, Eric
(NASA Glenn Research Center Cleveland, OH, United States)
Hardy, Richard L.
(NASA Johnson Space Center Houston, TX, United States)
Bollweg, Kenneth J.
(NASA Johnson Space Center Houston, TX, United States)
Ching, Michael
(Stellar Solutions, Inc. Greenbelt, MD, United States)
Date Acquired
February 27, 2019
Publication Date
September 18, 2018
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN61153
Meeting Information
Meeting: AIAA Space Forum
Location: Orlando, FL
Country: United States
Start Date: September 17, 2018
End Date: September 19, 2018
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: WBS 961866.01.01.04.22
Distribution Limits
Public
Copyright
Public Use Permitted.
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