attached reference space transportation system / expendable space transportation system / space transportation concepts / bank / friendly propulsion systems / gas generator / gas generator cycle / gas generator chamber / low cost manufacturing methods / gas-generator cycle / gas-side wall temperature nozzle stagnation temperature / maximum gas / fuel-rich gas generator / propulsion device / hot gas / engine solution / decreased technology / /
Organization
GTO mission / EPC / American Institute of Aeronautics and Astronautics / Internal Revenue Service / National Aeronautics and Space Administration / German Aerospace Center / /
Systems Analysis of a High Thrust, Low-Cost Rocket Engine Jens Kauffmann, Armin Herbertz, Martin Sippel Space Launcher Systems Analysis (SART), DLR, Cologne, Germany