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acceleration-deceleration accuracy air data quantities air data system aircraft AIRCRAFT ATTITUDE ambient pressure angle of attack angle of sideslip angle-of-attack parameter angle-of-sideslip parameter attack and sideslip calibration curve calibration data deg/sec determining angle differential pressure entry air data evaluation FADS pressures FADS test fices flight O Decreasing Flight Research Facility flight test flush air data flush orifices function of angle fuselage geometric altitude High Angles indicated Mach installed Kalman filter Langley Research Center Larson latitude angle Mach corrected Mach number measured at orifice NASA nose cap orifices orifices at station orifices located pacer pitot-static probe PP3ALL pressure altitude Pressure measured pressure orifices pressure ratios pulse-code modulation radar rawinsonde reference probe SEADS sensitivity to angle sensitivity to Mach sensor shown in figure shuttle entry air Siemers split-S stagnation pressure static-pressure position error Station 127 Station 61 transonic speeds Upper air analysis variations wind wind-tunnel