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This paper presents a sizing procedure for a rocket family capable of fulfilling multiple missions. It proposes an optimization formulation to enable cost savings by considering the commonalities between the vehicles.
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This page is a summary of: Simultaneous Sizing of a Rocket Family with Embedded Trajectory Optimization, Journal of Spacecraft and Rockets, January 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a35781.
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