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FY23 Descent Systems Study Annual Review Previous NASA studies of landing human-scale payloads on Mars have concluded that supersonic retropropulsion (SRP), or using multiple retrorocket engines beginning at supersonic descent conditions, is an enabling technology. DSS is partnering with the Aerosciences Evaluation and Test Capabilities (AETC) office to conduct a SRP test in the Langley Unitary Plan Wind Tunnel (UPWT) to quantify the SRP prediction capabilities of multiple computational fluid dynamics (CFD) solvers for a range of model configurations, thrust magnitudes, and tunnel conditions.
Document ID
20230013067
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Karl Edquist
(Langley Research Center Hampton, Virginia, United States)
Ashley Korzun
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
September 7, 2023
Subject Category
Aerodynamics
Meeting Information
Meeting: Game Changing Development FY23 Annual Program Review
Location: San Antonio, TX
Country: US
Start Date: September 18, 2023
End Date: September 22, 2023
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 335803.04.21.23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
Propulsive Descent
Supersonic Retropropulsion
FUN3D
OVERFLOW
Loci-CHEM
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