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Comparing Particle Flow Regimes in the L2K Arcjet with Martian Entry ConditionsIn this study, the US3D-DUST code will be used to simulate particles in the L2K dusty-flow test environments and compare them to conditions in the shock layer of the Schiaparelli capsule during its entry into the Martian atmosphere in 2016. The particle Reynolds, Mach, and Knudsen numbers, key non-dimensional numbers that characterize the dusty-flow environments, will be compared between the L2K and Martian shock layers. This study will provide a preliminary assessment of how well-suited L2K dusty-flow conditions are for particle drag model validation and the development of particle impact surface damage correlations. The results of this study may help to guide the design of future dusty flow environments in the L2K facility
Document ID
20220007187
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Grant Palmer
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Amal Sahai
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Dirk Allofs
(German Aerospace Center Cologne, Germany)
Ali Guelhan
(German Aerospace Center Cologne, Germany)
Date Acquired
May 9, 2022
Subject Category
Space Sciences (General)
Meeting Information
Meeting: 2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions & Engineering
Location: Heilbronnn
Country: DE
Start Date: June 19, 2022
End Date: June 23, 2022
Sponsors: European Space Agency
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Technical Management
Keywords
Dusty flow
Drag force
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