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Multidisciplinary Design of a RBCC SSTO using Taguchi Methods
(Georgia Institute of Technology, 1993-02)
This paper presents the results of an effort to optimize a conceptual design of a conical (winged- cone) single-stage-to-orbit launch vehicle. The vehicle employs a rocket-based combined-cycle (RBCC) engine capable of four ...
Results of a Rocket-Based Combined-Cycle SSTO Design Using Parametric; MDO Methods
(Georgia Institute of Technology, 1994-04)
This paper reports the results of the second phase of a research project to characterize and optimize the design of an advanced launch vehicle for human access to low earth orbit. The vehicle makes use of rocket-based ...