NASA NTRS · 19710029198
Space shuttle: Basic aerodynamic characteristics for three GAC reusable orbital spaceplane configurations, ROS-NBI, ROS-NB2, and ROSWB1 at 0.17 Mach number
Abstract
Low speed wind tunnel tests of 1/25 scale models of reusable orbital spaceplanes for subsonic aerodynamic data at Mach 0.17
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Jung, W., Carlucci, F.. 1971-08-01. Space shuttle: Basic aerodynamic characteristics for three GAC reusable orbital spaceplane configurations, ROS-NBI, ROS-NB2, and ROSWB1 at 0.17 Mach number. https://ntrs.nasa.gov/citations/19710029198
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