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2.8% Ares I Acoustic Reentry Wind Tunnel Model

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NASA

Nov 30, 2012
Image Article
scale model of Ares I in wind tunnel
Test to determine fluctuating pressure environments from a 2.8% scale Ares I first stage configuration to verify and update reentry aero acoustics environments.

Test to determine fluctuating pressure environments from a 2.8% scale Ares I first stage configuration to verify and update reentry aero acoustics environments.