| Space vehicle design MD Griffin AIAA, 2004 | 421 | 2004 |
| Using CubeSat/micro-satellite technology to demonstrate the Autonomous Assembly of a Reconfigurable Space Telescope (AAReST) C Underwood, S Pellegrino, VJ Lappas, CP Bridges, J Baker Acta Astronautica 114, 112-122, 2015 | 174 | 2015 |
| CubeSail: A low cost CubeSat based solar sail demonstration mission V Lappas, N Adeli, L Visagie, J Fernandez, T Theodorou, W Steyn, ... Advances in Space Research 48 (11), 1890-1901, 2011 | 167 | 2011 |
| Direct thrust measurement of a permanent magnet helicon double layer thruster K Takahashi, T Lafleur, C Charles, P Alexander, RW Boswell, M Perren, ... Applied Physics Letters 98 (14), 141503, 2011 | 160 | 2011 |
| Attitude control for small satellites using control moment gyros VJ Lappas, WH Steyn, CI Underwood Acta Astronautica 51 (1-9), 101-111, 2002 | 149 | 2002 |
| Performance characterization of a helicon double layer thruster using direct thrust measurements S Pottinger, V Lappas, C Charles, R Boswell Journal of Physics D: Applied Physics 44 (23), 235201, 2011 | 126 | 2011 |
| Spacecraft formation flying using Lorentz forces MA Peck, B Streetman, CM Saaj, V Lappas Journal of the British Interplanetary Society 60, 263-267, 2007 | 99 | 2007 |
| Design and testing of a control moment gyroscope cluster for small satellites V Lappas, WH Steyn, C Underwood Journal of Spacecraft and Rockets 42 (4), 729-739, 2005 | 97 | 2005 |
| Design and development of a gossamer sail system for deorbiting in low earth orbit JM Fernandez, L Visagie, M Schenk, OR Stohlman, GS Aglietti, ... Acta Astronautica 103, 204-225, 2014 | 82 | 2014 |
| Completely stripped solar sail concept using bi-stable reeled composite booms JM Fernandez, VJ Lappas, AJ Daton-Lovett Acta astronautica 69 (1-2), 78-85, 2011 | 74 | 2011 |
| Characterising wireless sensor motes for space applications T Vladimirova, CP Bridges, G Prassinos, X Wu, K Sidibeh, DJ Barnhart, ... Second NASA/ESA conference on adaptive hardware and systems (AHS 2007), 43-50, 2007 | 74 | 2007 |
| Survey of technology developments in flywheel attitude control and energy storage systems V Lappas, D Richie, C Hall, J Fausz, B Wilson Journal of guidance, control, and dynamics 32 (2), 354-365, 2009 | 69 | 2009 |
| Torque amplification of control moment gyros VJ Lappas, WH Steyn, CI Underwood Electronics Letters 38 (15), 1, 2002 | 67 | 2002 |
| A control moment gyro (CMG) based attitude control system (ACS) for agile small satellites VJ Lappas PQDT-UK & Ireland, 2002 | 59 | 2002 |
| Solar sails: technology and demonstration status L Johnson, R Young, N Barnes, L Friedman, V Lappas, C McInnes International journal of aeronautical and space sciences 13 (4), 421-427, 2012 | 56 | 2012 |
| Practical results on the development of a control moment gyro based attitude control system for agile small satellites VJ Lappas | 53 | 2002 |
| A practical small satellite variable-speed control moment gyroscope for combined energy storage and attitude control DJ Richie, VJ Lappas, G Prassinos Acta Astronautica 65 (11-12), 1745-1764, 2009 | 52 | 2009 |
| Spacecraft swarm navigation and control using artificial potential field and sliding mode control CM Saaj, V Lappas, V Gazi 2006 IEEE International Conference on Industrial Technology, 2646-2651, 2006 | 52 | 2006 |
| Drag sails for space debris mitigation L Visagie, V Lappas, S Erb Acta Astronautica 109, 65-75, 2015 | 49 | 2015 |
| Redundant reaction wheel torque distribution yielding instantaneous l2 power-optimal spacecraft attitude control H Schaub, VJ Lappas Journal of guidance, control, and dynamics 32 (4), 1269-1276, 2009 | 49 | 2009 |
