Shuttle derivatives have been under study by the National Aeronautics and Space Administration (NASA) for a number of years. With Space Station Freedom and the Lunar/Mars Initiative established as national objectives, the demand for access to earth orbit is accelerating. These objectives have resulted in efforts to address additional launch requirements that must be met as the turn of the century approaches. Among the top level requirements are increased safety, higher reliability, lower cost, and the need for heavy lift launch capability. To satisfy these requirements, some of the largest technology demands will be placed upon the propulsion systems. Shuttle derived manned concepts are presented and the associated propulsion issues which arise from the top level requirements are discussed. These concepts are presented in terms of an overall architecture which can be achieved with modest up-front development.
Shuttle derived manned transportation systems
1991-05-01
Conference paper
No indication
English
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