Review of inflatable booms for deployable space structures: packing and rigidization M Schenk, AD Viquerat, KA Seffen, SD Guest Journal of Spacecraft and Rockets 51 (3), 762-778, 2014 | 337 | 2014 |
InflateSail de-orbit flight demonstration results and follow-on drag-sail applications C Underwood, A Viquerat, M Schenk, B Taylor, C Massimiani, R Duke, ... Acta Astronautica 162, 344-358, 2019 | 73 | 2019 |
Reactive collision avoidance for unmanned aerial vehicles using doppler radar A Viquerat, L Blackhall, A Reid, S Sukkarieh, G Brooker Field and service robotics: results of the 6th international conference, 245-254, 2008 | 71 | 2008 |
Bistable over the whole length (BOWL) CFRP booms for solar sails JM Fernandez, A Viquerat, VJ Lappas, AJ Daton-Lovett Advances in solar sailing, 609-628, 2014 | 57 | 2014 |
Functional and qualification testing of the InflateSail technology demonstrator A Viquerat, M Schenk, V Lappas, B Sanders 2nd AIAA Spacecraft Structures Conference, 1627, 2015 | 51 | 2015 |
Inflatable rigidisable mast for end-of-life deorbiting system A Viquerat, M Schenk, B Sanders, V Lappas European conference on spacecraft structures, materials and environmental …, 2014 | 50 | 2014 |
A plane symmetric 6R foldable ring AD Viquerat, T Hutt, SD Guest Mechanism and Machine Theory 63, 73-88, 2013 | 48 | 2013 |
Natural frequency optimization of braided bistable carbon/epoxy tubes: Analysis of braid angles and stacking sequences C Wu, A Viquerat Composite Structures 159, 528-537, 2017 | 40 | 2017 |
Tip force during blossoming of coiled deployable booms A Hoskin, A Viquerat, GS Aglietti International Journal of Solids and Structures 118, 58-69, 2017 | 39 | 2017 |
Cycloaliphatic epoxy-based hybrid nanocomposites reinforced with POSS or nanosilica for improved environmental stability in low Earth orbit A Suliga, I Hamerton, A Viquerat Composites Part B: Engineering 138, 66-76, 2018 | 38 | 2018 |
Analysis of atomic oxygen and ultraviolet exposure effects on cycloaliphatic epoxy resins reinforced with octa-functional POSS A Suliga, EM Jakubczyk, I Hamerton, A Viquerat Acta Astronautica 142, 103-111, 2018 | 34 | 2018 |
Blossoming analysis of composite deployable booms S Wang, M Schenk, S Jiang, A Viquerat Thin-Walled Structures 157, 107098, 2020 | 24 | 2020 |
Curved bistable composite slit tubes with positive Gaussian curvature G Knott, A Viquerat AIAA Journal 56 (4), 1679-1688, 2018 | 21 | 2018 |
Development of cycloaliphatic epoxy-POSS nanocomposite matrices with enhanced resistance to atomic oxygen MY Rivera Lopez, JM Lambas, JP Stacey, S Gamage, A Suliga, ... Molecules 25 (7), 1483, 2020 | 20 | 2020 |
Computational and experimental study on dynamic instability of extended bistable carbon/epoxy booms subjected to bending C Wu, A Viquerat Composite Structures 188, 347-355, 2018 | 18 | 2018 |
The InflateSail CubeSat mission: The first European demonstration of drag-sail de-orbiting C Underwood, A Viquerat, M Schenk, S Fellowes, B Taylor, C Massimiani, ... Volume 163 of the Advances in the Astronautical Sciences Series: Fourth IAA …, 2017 | 18 | 2017 |
Demonstrator flight missions at the Surrey space centre involving Gossamer sails V Lappas, J Fernandez, L Visagie, O Stohlman, A Viquerat, G Prassinos, ... Advances in Solar Sailing, 153-167, 2014 | 18 | 2014 |
Tip force and pressure distribution analysis of a deployable boom during blossoming S Wang, M Schenk, H Guo, A Viquerat International Journal of Solids and Structures 193, 141-151, 2020 | 16 | 2020 |
Natural frequency optimization and stability analysis of bistable carbon fiber reinforced plastic booms for space applications C Wu, A Viquerat, G Aglietti 3rd AIAA spacecraft structures conference, 1472, 2016 | 16 | 2016 |
Helical bistable composite slit tubes G Knott, A Viquerat Composite Structures 207, 711-726, 2019 | 15 | 2019 |