{"id":6525,"date":"2018-06-25T06:23:00","date_gmt":"2018-06-25T05:23:00","guid":{"rendered":"http:\/\/uosdesign.org\/designshow2018\/?page_id=6525"},"modified":"2020-07-13T12:10:28","modified_gmt":"2020-07-13T11:10:28","slug":"aero-astro-engineering","status":"publish","type":"page","link":"https:\/\/uosdesign.org\/designshow2020\/aero-astro-engineering\/","title":{"rendered":"Aero\/ Astro Engineering"},"content":{"rendered":"

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Aeronautics & Astronautics<\/h2>\t<\/div>\t<\/div>\n<\/div>\n
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Asymmetric UAV<\/h3>\n

Exploded assembly of the UAV   Wind tunnel test   Aircraft take-off<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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Ground Effect UAV<\/h3>\n

UAV final design CFD – Vortex tacking analysis   CFD – Static pressure plot<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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NHS Drone Logistics<\/h3>\n

Exploded render of Pelargos Exploded render of Pelargos (annotated)   Supply chain vision flow map   Cumulative sample arrival at SGH throughout the day   wind tunnel testing wind tunnel testing Isometric render of Pelargos<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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SIRIUS<\/h3>\n

SIRIUS in assembly Cutaway render 1 \u00a0 HTP oxidiser injector plate2 \u00a0 PX3 catalyst decompossition chamber3\u00a0\u00a0 Turpentine fuel injector4\u00a0\u00a0 Regeneratively-cooled Inconel nozzle  <\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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IPANEMA<\/h3>\n

Anottated final design Dual fuel system configuration   Final design proposal exploded view Final design proposal exploded view Prototype Prototype<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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Handheld Plasma Jet<\/h3>\n

CAD Render of the final product design CAD Render of interior components   Cut-through CAD render of final design Annotated exploded render   Plasma Jet observed during preliminary testing<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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ADMIRE<\/h3>\n

  Exploded view of the UAV 1 \u2013 Nose2 \u2013 Nose Attachment3 \u2013 Fuselage Extension (increased working area for the electronics)4 \u2013 Fuselage\/Wind Tunnel Attachment5 \u2013 Wing\/Fuselage Attachment6 \u2013 Supporting Rib7 \u2013 Backcone Attachment8 \u2013 Backcone9 \u2013 Horizontal Stabilizer\/Vertical Stabilizer Attachment   UAV Mounted on the Dynamic Attachment UAV Mounted […]<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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Wind Tunnel Model and Control System<\/h3>\n

Plan view of the Model \u2013 Cutaway to show Electronic and Mechanical Systems Cutaway to show Electronic and Mechanical Systems 1 High performance Data aquisition package2 FE validated metal constrction with rapidly modifiable modular geometry3 Roll mechanism incorporating high-thrust linear actuator and double-plated rocker mechanism4 Attitude measurement by infrared sensors […]<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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ASRV<\/h3>\n

Render of a \u2018V2\u2019 commercial concept for ASRV Render of the exploded \u2018V1\u2019 prototype design for ASRV, with translucent casing Annotated render of the exploded \u2018V1\u2019 prototype design for ASRV<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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SUBLIME<\/h3>\n

Top view of gondola Bottom view of gondola Proposed system design<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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Project Angel<\/h3>\n

Annotated final design concept The final design concept in a stowed configuration  <\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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RECONANCHOR<\/h3>\n

Installation configuration of RECONANCHOR   Deployed configuration of RECONANCHOR   Installation sequence for RECONANCHOR<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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UoS Small Satellite<\/h3>\n

Exploded CubeSat annotated CubeSat Antenna Deployment Testing in Thermal Chamber CubeSat Antenna Deployment Testing in Thermal Chamber CubeSat Testing in Thermal-Vacuum Chamber CubeSat System-level Test setup Assembled CubeSat<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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UK CanSat Project: MASS<\/h3>\n

Render of final CanSat modular design<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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Olympus Rover Trials<\/h3>\n

Photograph of Phobos 2020 physical prototype   Rover exploring rough terrain   Demonstration of rough terrain traversing capabilities   Demonstration of wheel gimballing system   3D-printed locomotion and arm subsystem   Internal view of the rover chassis, showing electronics     CAD rendering of rover arm assembly Exploded view of […]<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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Human Powered Aircraft<\/h3>\n

Test fitting of the modular aircraft wing demonstrates the scale of the wing   Pilot\u2019s fairing   Lazarus propellor blade showing 3D printed sections<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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Formula Student – STAG VII<\/h3>\n

Side render of STAG VII Rear 3\/4 view render of STAG VII Driver view Render of inderside of STAG VII<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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Biomimicry Inspired Fixed Wing UAV<\/h3>\n

Front view of aircraft assembly     Exploded view of aircraft1. Multi-Element Winglets2. Modular Winglet Housing3. V-Tail Assembly4. Carbon Fibre Fuselage Panels5. Aluminium Fuselage Ribs6. Electronics Assembly7. Electric Ducted Fan   Furling winglet and tiperon assembly   Mark 1 winglet configuration mounted in the wind tunnel   Mark 1 clean […]<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n \n

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US CanSat Project: Team Aether<\/h3>\n

CanSat delta-wing glider CanSat glider deployment   CanSat glider and wing deployment   CanSat stowed glider configuration<\/p>\n \n\n \n Read More <\/span>\n <\/div>\n <\/div>\n\n \n \"\"\n \n <\/a>\n\n \n <\/article>\n\n \n <\/div>\n\n\n \n\n \n\n \n<\/div>\n\t

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CanSat delta-wing glider CanSat glider deployment   CanSat glider and wing deployment   CanSat stowed glider configuration<\/p>\n","protected":false},"author":1,"featured_media":0,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"page-templates\/full-width-builder.php","meta":[],"_links":{"self":[{"href":"https:\/\/uosdesign.org\/designshow2020\/wp-json\/wp\/v2\/pages\/6525"}],"collection":[{"href":"https:\/\/uosdesign.org\/designshow2020\/wp-json\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/uosdesign.org\/designshow2020\/wp-json\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/uosdesign.org\/designshow2020\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/uosdesign.org\/designshow2020\/wp-json\/wp\/v2\/comments?post=6525"}],"version-history":[{"count":2,"href":"https:\/\/uosdesign.org\/designshow2020\/wp-json\/wp\/v2\/pages\/6525\/revisions"}],"predecessor-version":[{"id":7173,"href":"https:\/\/uosdesign.org\/designshow2020\/wp-json\/wp\/v2\/pages\/6525\/revisions\/7173"}],"wp:attachment":[{"href":"https:\/\/uosdesign.org\/designshow2020\/wp-json\/wp\/v2\/media?parent=6525"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}