HIGHLIGHTS
- who: Pedro Orgeira-Crespo and colleagues from the Department of Mechanical Engineering, Heat Engines and Machines and Fluids, Aerospace Engineering have published the Article: Optimization of the Conceptual Design of a Multistage Rocket Launcher, in the Journal: Aerospace 2022, 286 of /2022/
- what: The authors propose software for the separate optimization of the trajectory of a launch maximizing the payload weight and the global design while varying the power plant selection. The authors chose to use the genetic algorithm to solve the optimization design problem (including the distribution of masses), whilst for the optimization of . . .
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