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12 Figure 50 Abort 65-sec aborts 70 Figure abort is possible aborts 14 Figure angle for HL-20 angle versus ascent trajectory Axial load factor bank angle Basic HL-20 vehicle boundary conditions cost function drag coefficient dynamic pressure equality and inequality final altitude final velocity flat Earth flight path angle ft/sec given by equation heading angle HL-20 lifting body HL-20 RTLS abort inequality constraint vectors Kennedy Space Center lift coefficient lift force load factor versus lower body flaps Mach number maximum trim NASA nonlinear programming problem OMS fuel optimal control problem optimal control theory optimal state rates Orbital Maneuvering System Personnel Launch System reference rotated drag polar RTLS abort 12 RTLS problem runway sec Figure set of attainability Shuttle Landing Facility skid strip SRM's sustainer SRM burn Table three-dimensional hodograph Titan III two-dimensional hodograph U.S. Standard Atmosphere upper body flaps values wing flaps