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Space shuttle: Basic aerodynamic characteristics for three GAC reusable orbital spaceplane configurations, ROS-NBI, ROS-NB2, and ROSWB1 at 0.17 Mach number

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Abstract

Low speed wind tunnel tests of 1/25 scale models of reusable orbital spaceplanes for subsonic aerodynamic data at Mach 0.1

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    Last time updated on 02/09/2017