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Space Shuttle Orbiter trimmed center-of-gravity extension study. Volume 9: Effects of configuration modifications on the aerodynamic characteristics of the 140 A/B Orbiter at Mach numbers of 1.5, 2.0, and 2.5. [wind tunnel tests

W. Pelham Phillips, R. H. Fournier

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Key concepts: Orbiter, Space Shuttle, Mach number, Aerospace engineering, Aerodynamics, Aeronautics, Volume (thermodynamics), Center of gravity

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Space Shuttle Orbiter trimmed center-of-gravity extension study. Volume 9: Effects of configuration modifications on the aerodynamic characteristics of the 140 A/B Orbiter at Mach numbers of 1.5, 2.0, and 2.5. [wind tunnel tests — Research Paper | ScholarLens