Print Email Facebook Twitter A feasibility study on the recovery of Electron's first stage using a vertical landing approach Title A feasibility study on the recovery of Electron's first stage using a vertical landing approach Author Hoefsloot, Stijn (TU Delft Aerospace Engineering) Contributor Naeije, M.C. (mentor) Degree granting institution Delft University of Technology Programme Aerospace Engineering Date 2022-06-22 Abstract The small satellite market is rapidly growing and becomes more competitive by the day. In order to reduce launch costs, the concept of reusable launch vehicles wins popularity. Only few companies have managed to successfully recover and re-use their launch vehicle, of which SpaceX is the only one using a powered descent technique. This study focuses on applying that same technique on a small satellite launcher: Rocket Labs Electron. A 3-DOF trajectory optimization is performed to find the fuel optimal ascent and descent trajectories of the Electron. The original design of the Electron is adhered to as much as possible. The optimization is performed for a variety of Single- and Multi objective optimizers and different settings. Although this is only a feasibility study in which many assumptions are made, the results look promising for further research to be done. Subject RecoveryFirst StagePowered DescentTrajectory Optimization To reference this document use: http://resolver.tudelft.nl/uuid:a04f4604-e06a-4fc7-b883-6fe52f32cccf Part of collection Student theses Document type master thesis Rights © 2022 Stijn Hoefsloot Files PDF Master_Thesis_Electron_Recovery.pdf 10.71 MB Close viewer /islandora/object/uuid:a04f4604-e06a-4fc7-b883-6fe52f32cccf/datastream/OBJ/view