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The optimization of ascent trajectory and the design of the stage thrust law are generally done independently. We show how the process can be integrated for improved performance.
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This page is a summary of: Integrated Optimization of First-Stage SRM and Ascent Trajectory of Multistage Launch Vehicles, Journal of Spacecraft and Rockets, April 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34930.
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