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Transformational Propulsion for In-Space Fast TransitsNASA has ambitious mission objectives requiring much faster transits to and from Mars, interstellar probes and a gravity lens observatory. However, there has been very little investment in transformational propulsion system development activities since the 1970s. There have been dozens of concepts proposed for high acceleration propulsion solutions, but nearly all have been limited to paper studies. A quick assessment was completed in 2023 to determine the potential of transformational propulsion concepts to enable faster transits, with a focus on crewed missions to and from Mars. Far-term conventional nuclear thermal propulsion is limited to very modest improvement in transfer times. Advanced nuclear propulsion options have significant performance potential, but limited interim evolutionary payoff for NASA. Advanced electric propulsion, both solar and nuclear, offers transformational performance potential with high payoff during interim progress for power production, conversion, and heat rejection technologies. Study results and recommendations for near-term investments are presented herein.
Document ID
20230017672
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
John W. Dankanich
(Marshall Space Flight Center Redstone Arsenal, United States)
John A. Carr
(Marshall Space Flight Center Redstone Arsenal, United States)
Laura M. Burke
(Glenn Research Center Cleveland, United States)
Geoffrey A. Landis
(Glenn Research Center Cleveland, United States)
Timothy J. Peshek
(Glenn Research Center Cleveland, United States)
Zachary C. Zoloty
(Glenn Research Center Cleveland, United States)
Robert C. O'Brien
(Idaho National Laboratory Idaho Falls, United States)
Date Acquired
December 4, 2023
Subject Category
Astrodynamics
Meeting Information
Meeting: AIAA SciTech Forum and Exposition
Location: Orlando, FL
Country: US
Start Date: January 8, 2024
End Date: January 12, 2024
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 600566.10.62
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
Propulsion
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