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A/R SSTO vehicle aerodynamic Aeronautics and Astronautics Aerospatiale AIAA AIAA Paper air intake airbreathing propulsion American Institute analysis angle ATREX axisymmetric baseline boundary layer calculations coefficient combustion combustor compression computational concept configuration cowl duct efficiency equations experimental Figure flight testing flow field forebody free stream fuel grid heat loads hydrogen HYPERSONICS TECHNOLOGIES CONFERENCE injection Institute of Aeronautics integration interaction INTERNATIONAL AEROSPACE PLANES launch vehicle launcher leading edge Mach number mass measurements mixing mode module NASA NASP nozzle oblique shock operation optimization orbit Oryol parameters payload performance pitot pressure PLANES AND HYPERSONICS predict propulsion system ramjet ramp ratio Research reusable rocket engines scramjet shock tunnel shock wave simulation slit space transportation systems Spaceplane specific impulse SSTO structure supersonic surface take-off tank temperature thermal management throat thrust total pressure TSNIIMASH TSTO turbulent unstart velocity viscous VITMAC Volvo Aero waverider weight