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New Magnetohydrodynamic (MHD) Lift Concept for More Efficient Missions to Mars and NeptuneThe potential for using an applied magnetic field to augment the aerodynamic lift and drag of a hypersonic vehicle entering Neptune or Mars was studied. The study was conducted to assess whether magnetohydrodynamics (MHD)could boost aerodynamic lift and/or drag for aerocapture of a spacecraft into planetary orbit. MHD seemed well suited to create Lorentz forces during aerocapture when the flow is most ionized and conductive. Neptune and Mars were selected since larger payloads and faster trip times to each planet may substantially increase scientific and exploration opportunities. The results of the systems analysis presented herein suggest that a single MHD effector located off-centerline creates steering forces equaling whole-body aerodynamic forces and suggests a ground-breaking opportunity for new mission classes. The magnetic field required to produce these large forces is around 1 Tesla (T) having a mass roughly the same amount as the ballast used for recent Mars lander missions.
Document ID
20210024776
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Robert W Moses
(Langley Research Center Hampton, Virginia, United States)
F Mcneil Cheatwood
(Langley Research Center Hampton, Virginia, United States)
Christopher O Johnston
(Langley Research Center Hampton, Virginia, United States)
Sergey O Macheret
(Purdue University West Lafayette West Lafayette, Indiana, United States)
Bernard Parent
(University of Arizona Tucson, Arizona, United States)
Justin Little
(University of Washington)
Matthew Austin
(Florida Institute of Technology Melbourne, Florida, United States)
Andrew Aldrin
(Florida Institute of Technology Melbourne, Florida, United States)
Justin S Green
(Langley Research Center Hampton, Virginia, United States)
R Anthony Williams
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
November 22, 2021
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: AIAA SciTech Forum
Location: San Diego, CA
Country: US
Start Date: January 3, 2022
End Date: January 7, 2022
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: 80HQTR19NOA01-20NIAC-A1
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Professional Review
Keywords
Aerocapture
Neptune
Mars
Fast Arrival
Fast Transits
Magnetohydrodynamic
MHD effector
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