Static and Control Investigations of an 0.030-Scale Space Shuttle Orbiter Configuration 140A/B Model in the Ames Research Center 11 by 11-Foot Transonic Wind Tunnel (Oa53a), Volume 1
Static and Control Investigations of an 0.030-Scale Space Shuttle Orbiter Configuration 140A/B Model in the Ames Research Center 11 by 11-Foot Transonic Wind Tunnel (Oa53a), Volume 1
- New search for: M. E. Nichols
- New search for: M. E. Nichols
A wind tunnel test of an 0.030 scale model of the Rockwell International Configuration 140A/B Space Shuttle Vehicle Orbiter were conducted in the Ames Research Center 11- by 11-Foot Transonic Wind Tunnel. This part (part A) of test series 0A53 was conducted at Mach numbers of 0.6, 0.8, 0.9, 1.05, and 1.20, and at Reynolds numbers from 1.8 x to 6.5 million per foot. The objective of this test was to establish and verify longitudinal and lateral-directional aerodynamic performance, stability, and control characteristics for the Configuration 140A/B SSV Orbiter. Reynolds number studies were performed for certain nominal control-settings. An alternate leading-edge wing configuration and sealed elevon-split arrangement were tested. Bodyflap, elevon, speedbrake, and rudder hinge moments were measured in addition to standard six-component forces and moments and base pressure data. Furthermore, six-component force and moment data were measured for the vertical tail assembly. (Author)
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Static and Control Investigations of an 0.030-Scale Space Shuttle Orbiter Configuration 140A/B Model in the Ames Research Center 11 by 11-Foot Transonic Wind Tunnel (Oa53a), Volume 1
1974
974 pages
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English