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Current Capabilities of AFRL’s Spacecraft Simulation ToolAssessment of spacecraft integration issues is typically accomplished with a combination of
numerical tools developed to simulate different regions with different key physics. For instance,
a detailed study of spacecraft with an electric propulsion device requires a device model, a plume model, and a spacecraft charging model. AFRL’s in-house spacecraft simulation tool, TURF, is now capable of performing all of these calculations in one simulation. In addition, the plume simulation capability has been expanded significantly to improve speed and accuracy. Other upgrades in TURF include adaptive mesh refinement (AMR) and dynamic load balancing. All of these upgrades are covered in this paper by providing detailed descriptions or pointing to relevant references. This paper also presents three example simulations demonstrating its multi-physics multi-scale capability.
Document ID
20220008291
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Samuel J. Araki
(Edwards Air Force Base Edwards Air Force Base, California, United States)
Robert S. Martin
(Edwards Air Force Base Edwards Air Force Base, California, United States)
David L. Bilyeu
(Edwards Air Force Base Edwards Air Force Base, California, United States)
Lubos Brieda
(Particle In Cell Consulting LLC.)
Carrie Hill
(Aurora Engineering)
Maria Choi
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
May 26, 2022
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: 37th International Electric Propulsion Conference
Location: Boston, MA
Country: US
Start Date: June 19, 2022
End Date: June 23, 2022
Sponsors: Accion International, Enpulsion
Funding Number(s)
WBS: 837933.06.03.02.03
CONTRACT_GRANT: SPEC5721
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
spacecraft simulation
Hall thruster plume
Electron Fluid Model
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