2.8% Ares 1 Acoustic Reentry Wind Tunnel Model2.8% 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 Facebook Pinterest X LinkedIn Email https://www.nasa.gov/image-detail/645252main_acd08-0266-019_1600_full/Copy URL to clipboard> DownloadShareTagsWebMod GrandfatheredImage CreditNASASize1600x1200px