Marshall Space Flight Center / transportation system SpaceLiner / Space Transportation System Research and Development Center / American Institute of Aeronautics / /
IndustryTerm
large turbine gas / turbo machinery efficiency / turbine gas flow rate / hot fuel gas / turbine gas temperature / ultrafast passenger transportation system / turbine gas mass flow / turbine gas mass flow rate / fuel rich combustion gas / oxygen rich gas / turbo machinery design / machinery / gas hydrogen / turbo machinery design parameter / turbo machinery pre-sizing / higher turbine gas pressure / gas oxygen / turbine gas / fuel rich gas / machinery pre-sizing / turbo machinery / hot gas / turbine gas pressure / preferred design solution / larger turbine gas / /
NaturalFeature
OTP / LPFTP / /
Organization
Space Transportation System Research and Development Center / SLME V / Space Flight Center / American Institute of Aeronautics and Astronautics / NS NS / National Aeronautics and Space Administration / USAF / /
Person
Martin Sippel / Turbine Entry / Ryoma Yamashiro / /
Position
fuel head / stage Head / Marshall / SSME power-head / /
IAC-12-C4.1.11 PRELIMINARY DESIGN STUDY OF STAGED COMBUSTION CYCLE ROCKET ENGINE FOR SPACELINER HIGH-SPEED PASSENGER TRANSPORTATION CONCEPT