NASA NTRS · 20210024567
A New Flow-Through Balance for Retropropulsion Testing
Abstract
Supersonic 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.
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Devin E Burns, Peter A Parker, Christopher M Cagle, Veronica M Hawke, Kenneth G Toro, William L Kleb. A New Flow-Through Balance for Retropropulsion Testing. https://ntrs.nasa.gov/citations/20210024567
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