| Investigation on the dynamic response of blades with asymmetric under platform dampers A Bessone, F Toso, T Berruti Turbo Expo: Power for Land, Sea, and Air 56772, V07BT33A003, 2015 | 24 | 2015 |
| Multi-objective optimal control of the ascent trajectories of launch vehicles LA Ricciardi, M Vasile, F Toso, CA Maddock AIAA/AAS Astrodynamics Specialist Conference, 5669, 2016 | 12 | 2016 |
| Vehicle and mission design of a future small payload launcher C Maddock, F Toso, L Ricciardi, A Mogavero, KH Lo, S Rengarajan, ... 21st AIAA International Space Planes and Hypersonics Technologies Conference …, 2017 | 9 | 2017 |
| Optimisation of ascent and descent trajectories for lifting body space access vehicles F Toso, A Riccardi, E Minisci, CA Maddock 66th International Astronautical Congress, IAC2015, 1-12, 2015 | 7 | 2015 |
| How to launch small payloads? Evaluation of current and future small payload launch systems S McIntyre, T Fawcett, T Dickinson, CA Maddock, A Mogavero, L Ricciardi, ... 14th Reinventing Space Conference, 2016 | 6 | 2016 |
| Launch abort trajectory optimisation for reusable launch vehicles F Toso, CA Maddock 21st AIAA International Space Planes and Hypersonics Technologies Conference …, 2017 | 5 | 2017 |
| A commercially driven design approach to UK future small payload launch systems S McIntyre, T Fawcett, T Dickinson, M West, CA Maddock, A Mogavero, ... 14th Reinventing Space Conference, 2016 | 4 | 2016 |
| Deployed payload analysis for a single stage to orbit spaceplane F Toso, CA Maddock 67th International Astronautical Congress, 2016 | 3 | 2016 |
| Initial guess generation strategies for spaceplane trajectory optimisation F Toso, C Maddock Transactions of the Japan Society for Aeronautical and Space Sciences, 2017 | 2 | 2017 |
| Multidisciplinary design analysis of a semi-reusable two-stage-to-orbit small payload launch system C Maddock, LA Ricciardi, F Toso, M Vasile International Astronautical Congress 2019, 2019 | 1 | 2019 |
| Comparison of the emissions of current expendable launch vehicles and future spaceplanes RJ Garner, F Toso, CA Maddock 67th International Astronautical Congress, 1-12, 2016 | 1 | 2016 |
| Multidisciplinary Design Optimisation for Missionisation of Re-entry Vehicles: Preliminary Mission Design and Mission Capabilities Evaluation of Winged Re-Entry Vehicles Case Study J Guadagnini, G De Zaiacomo, F Toso 12th International Conference on Guidance, Navigation & Control Systems (GNC …, 2023 | | 2023 |
| Preliminary design of reusable future space access vehicles F Toso | | 2023 |
| Lessons learned from the first student-led Sapienza GEA cave exploration analog mission P Marzioli, A Fabbrizi, L Chiavari, A Di Giacomo, C Ghini, A Binni, ... Proceedings of the International Astronautical Congress, IAC, 1-5, 2022 | | 2022 |
| Launch Collision Avoidance Sensitivity Analysis G Falco, F Toso, A Ratcliffe, N Sánchez-ortiz 8th European Conference on Space Debris 8 (1), 2021 | | 2021 |
| Comparison of the emissions of current expendable launch vehicles and future spaceplanes. In: 67th International Astronautical Congress, 2016 RJ Garner, F Toso, CA Maddock | | |
