2.8% Ares 1 Acoustic Reentry Wind Tunnel Model
2.8% Ares 1 Acoustic Reentry Wind Tunnel Model Test to determine fluctuating pressure environments from a 2.8% scale Ares I first stage configuration to verify and update reentry aero acoustics environments.
Image Credit: NASA
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https://www.nasa.gov/image-detail/645252main_acd08-0266-019_1600_full/
Image CreditNASA
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