NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
A New Flow-Through Balance for Retropropulsion TestingSupersonic retropropulsion is believed to be an enabling technology for large-scale human Mars lander vehicle concepts. Ground testing of such vehicles requires the development of new flow-through wind tunnel balances because no suitable balances exist. A new flow-through balance is designed that employs membranes in place of bellows, which have historically been used, and that passes the flow through load bearing parts of the balance. Flow through the balance is optimized via the addition of flow guides, which are manufactured as separate parts, and attached to the balance. Calibration of this new flow-through balance demonstrates that it can suitably characterize the load and pressure ranges it was designed for, which provides aero researchers a new tool to directly measure supersonic retropropulsion performance of powered descent vehicles.
Document ID
20210024567
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Devin E Burns
(Langley Research Center Hampton, Virginia, United States)
Peter A Parker
(Langley Research Center Hampton, Virginia, United States)
Christopher M Cagle
(Langley Research Center Hampton, Virginia, United States)
Veronica M Hawke
(Science and Technology Corp. Moffett Field, CA, United States)
Kenneth G Toro
(Langley Research Center Hampton, Virginia, United States)
William L Kleb
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
November 18, 2021
Subject Category
Aeronautics (General)
Meeting Information
Meeting: 2022 AIAA SciTech Forum
Location: San Deigo, CA
Country: US
Start Date: January 3, 2022
End Date: January 7, 2022
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 951888.03.07.04.03
Distribution Limits
Public
Copyright
Public Use Permitted.
Patent
[SG Note: non-provisional patent application filed on August 30,2021]
Patent Application
Technical Review
Single Expert
Keywords
Flow through balance
Retropropulsion
Human Mars lander
Ground Testing
No Preview Available