This paper introduces an evolvable Space Shuttle derived family of launch vehicles. It details the steps in the evolution of the vehicle family, noting how the evolving lift capability compares with the evolving lift requirements. A system description is given for each vehicle. The cost of each development stage is described. Also discussed are demonstration programs, the merits of the SSME vs. an expendable rocket engine (RS-68), and finally, the next steps needed to refine this concept.
Shuttle Derived In-Line Heavy Lift Vehicle
AIAA Conference ; 2005 ; Tucson, AZ, United States
2005-01-01
Preprint
No indication
English
Shuttle Derived In-Line Heavy Lift Vehicle
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