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42nd CONGRESS abort aerodynamic Aerospace Aerospike engine altitude AMLS analysis angle ARIANE ascent battery booster capability cargo cavity concept configuration cost crew efficiency electrical energy engine environment facilities flight fuel ground helium Hotol hybrid hydrogen hypersonic integration International Astronautical Federation landing launch processing Launch System launch vehicle launcher liquid load Logistics Vehicle Low Earth Orbit Mach mass mission NASA near-term nozzle nuclear propulsion operations optimized options orbit P/A module payload performance phase power system propellant propulsion system PVCC ramjet ratio recovery reduced reentry reusable rocket runway satellite second stage simulation solar array solar cells Space Shuttle Space Station Space Station Freedom space transportation spacecraft specific impulse SSME SSTO structure subsystem surface takeoff tank temperature tests thermal thrust trajectory TSTO two-stage unmanned upper stage velocity voltage VT-SSTO VTVL weight wing