https://peertube.dngr.us/videos/watch/11dd37df-5f18-4486-94ec-1855eccc89e9 Attached inflatable decelerators (AID) were tested in an environmental chamber, a spin tunnel, and a wind tunnel. Deployment tests were conducted in environmental chamber to examine guided and unguided water alcohol vapor inflation. Subsonic performance tests were conducted in the spin tunnel. The full-scale wind tunnel was used for AID gust and supersonic performance tests. The supersonic tests were conducted at Mach number 3.0 with 12 ounces of fluid and Mach number 2.2 with six ounces of fluid. Related to: http://hdl.handle.net/2060/19700018039 Mirrored from YouTube: https://youtu.be/uUR6bFN3IMA Original channel: NASA STI Program Wed, 15 Jul 2026 11:50:55 GMT https://validator.w3.org/feed/docs/rss2.html PeerTube - https://peertube.dngr.us https://peertube.dngr.us/lazy-static/avatars/ec5edb1e-3795-4978-be4f-c67e98fbc992.png https://peertube.dngr.us/videos/watch/11dd37df-5f18-4486-94ec-1855eccc89e9 All rights reserved, unless otherwise specified in the terms specified at https://peertube.dngr.us/about and potential licenses granted by each content's rightholder.