preliminary turbo-machinery sizing / oxidizer-rich preburner gas turbine / real gas effects / comfortable pressurized travel compartment / hot gas valve / fuel-rich preburner gas turbine / transportation / intercontinental travel / overall energy / porous ceramic media / machinery / required oxygen gas / long distance travel / earth-orbit space transportation / pressurization gas temperatures / numerical tools / high pressure hot gas lines / passenger transportation concept / intercontinental travel space tourism / sustainable low-cost space transportation / fuel tank pressurization gas / launcher hardware / active cooling systems / inhouse tool / Light-weight inflatable solutions / huge intercontinental travel / The hydrogen gas mass / down-range landing site / turbine gas / manufacturing / space transportation / oxidizer tank pressurization gas / preferred design solution / /
Organization
Europe mission / Reference mission / Congress / Federal Government / National Aeronautics and Space Administration / European Union / /
IAC-13-D2[removed]Progress of SpaceLiner Rocket-Powered High-Speed Concept