| The benefits of very low earth orbit for earth observation missions NH Crisp, PCE Roberts, S Livadiotti, VTA Oiko, S Edmondson, SJ Haigh, ... Progress in Aerospace Sciences 117, 100619, 2020 | 152 | 2020 |
| Spacecraft drag modelling DM Prieto, BP Graziano, PCE Roberts Progress in Aerospace Sciences 64, 56-65, 2014 | 104 | 2014 |
| Very Low Earth Orbit mission concepts for Earth Observation. Benefits and challenges. JV Llop, PCE Roberts, Z Hao, LR Tomas, V Beauplet Reinventing Space Conference 2014, 2014 | 84 | 2014 |
| SYSTEM ANALYSIS AND TEST-BED FOR AN ATMOSPHERE-BREATHING ELECTRIC PROPULSION SYSTEM USING AN INDUCTIVE PLASMA THRUSTER F Romano, T Binder, GH Herdrich, P Roberts, S Rodriguez-Donaire, ... International Astronautical Congress 2017, 2017 | 67 | 2017 |
| RF helicon-based inductive plasma thruster (IPT) design for an atmosphere-breathing electric propulsion system (ABEP) F Romano, YA Chan, G Herdrich, C Traub, S Fasoulas, PCE Roberts, ... Acta Astronautica 176, 476-483, 2020 | 65 | 2020 |
| Drag sail for end-of-life disposal from low earth orbit PCE Roberts, PG Harkness Journal of Spacecraft and Rockets 44 (6), 1195-1203, 2007 | 58 | 2007 |
| A review of gas-surface interaction models for orbital aerodynamics applications S Livadiotti, NH Crisp, PCE Roberts, SD Worrall, VTA Oiko, S Edmondson, ... Progress in Aerospace Sciences 119, 100675, 2020 | 51 | 2020 |
| System modelling of very low Earth orbit satellites for Earth observation NH Crisp, PCE Roberts, F Romano, KL Smith, VTA Oiko, V Sulliotti-Linner, ... Acta Astronautica 187, 475-491, 2021 | 46 | 2021 |
| Intake design for an atmosphere-breathing electric propulsion system (ABEP) F Romano, J Espinosa-Orozco, M Pfeiffer, G Herdrich, NH Crisp, ... Acta Astronautica 187, 225-235, 2021 | 43 | 2021 |
| In-orbit aerodynamic coefficient measurements using SOAR (Satellite for Orbital Aerodynamics Research) NH Crisp, PCE Roberts, S Livadiotti, AM Rojas, VTA Oiko, S Edmondson, ... Acta Astronautica 180, 85-99, 2021 | 42 | 2021 |
| Spacecraft drag modelling D Mostaza Prieto, BP Graziano, PCE Roberts Progress in Aerospace Sciences 64, 56-65, 2014 | 38 | 2014 |
| Atmospheric interface reentry point targeting using aerodynamic drag control J Virgili, PCE Roberts, NC Hara Journal of Guidance, Control, and Dynamics 38 (3), 403-413, 2015 | 37 | 2015 |
| On the exploitation of differential aerodynamic lift and drag as a means to control satellite formation flight C Traub, F Romano, T Binder, A Boxberger, GH Herdrich, S Fasoulas, ... CEAS Space Journal 12, 15-32, 2020 | 36 | 2020 |
| Discoverer-Radical redesign of earth observation satellites for sustained operation at significantly lower altitudes PCE Roberts, NH Crisp, S Edmondson, SJ Haigh, RE Lyons, VTA Oiko, ... Proceedings of the International Astronautical Congress, IAC 68, 9254-9262, 2017 | 33 | 2017 |
| Heliogyro solar sail with self-regulated centrifugal deployment enabled by an origami-inspired morphing reflector R Wu, PCE Roberts, C Soutis, C Diver Acta Astronautica 152, 242-253, 2018 | 29 | 2018 |
| The development of high fidelity linearized J2 models for satellite formation flying control JA Roberts, PCE Roberts AAS Paper, 04-162, 2004 | 28 | 2004 |
| DISCOVERER – Making Commercial Satellite Operations in Very Low Earth Orbit a Reality P Roberts, N Crisp, VT Abrao Oiko, S Edmondson, S Haigh, C Huyton, ... International Astronautical Congress 2019, 2019 | 27* | 2019 |
| Descending sun-synchronous orbits with aerodynamic inclination correction J Virgili Llop, PCE Roberts, K Palmer, S Hobbs, J Kingston Journal of Guidance, Control, and Dynamics 38 (5), 831-842, 2015 | 24 | 2015 |
| ΔDsat, a QB50 CubeSat mission to study rarefied-gas drag modelling J Virgili, PCE Roberts Acta Astronautica 89, 130-138, 2013 | 21 | 2013 |
| ADBSat: Methodology of a novel panel method tool for aerodynamic analysis of satellites LA Sinpetru, NH Crisp, D Mostaza-Prieto, S Livadiotti, PCE Roberts Computer Physics Communications 275, 108326, 2022 | 20 | 2022 |
Nicholas H CrispUniversity of ManchesterVerified email at manchester.ac.uk
