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Wind tunnel test of the 0.015-scale Rockwell International space shuttle vehicle orbiter in the Ames 6 by 6 foot supersonic wind tunnel. [to determine longitudinal and lateral-directional characteristics

M. D. Milam, T. J. Dziubala

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Key concepts: Orbiter, Wind tunnel, Space Shuttle, Engineering, Marine engineering, Aerospace engineering, Aeronautics, Supersonic speed

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Wind tunnel test of the 0.015-scale Rockwell International space shuttle vehicle orbiter in the Ames 6 by 6 foot supersonic wind tunnel. [to determine longitudinal and lateral-directional characteristics — Research Paper | ScholarLens