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5-per cent-chord line actual flight airplane oscillation angle of attack angle of sideslip area to wing artificial feel Aspect ratio attack of l0 boost with artificial center stick control deflection Control system Irreversible control task covered by fuselage damping ratio deg 0 Control deg/deg/sec deg/sec due to full fixed-base flight simulator flight condition flight envelope flight gain flight plan flight research flight-path angle ft-lb g units high-altitude hinge line horizontal tail hypersonic indicated inertia Irreversible hydraulic boost lb/sq ft Level flight lightly damped low dynamic pressure Mach number maximum Mean aerodynamic chord minimum dynamic pressure Movable surface area NASA normal acceleration North American Aviation pilot was requested pitch angle precise control pressure altitude pressure of l0.6 pull-up push-over reaction controls rocket engine roll control Root chord slug-ft Span stabilizer deflection stabilizing the airplane system Irreversible hydraulic Taper ratio Tip chord trajectory velocity wing area X-l5 airplane X-l5 flight