Towards a common transportation layer. A resilient, rapid-response and precise transportation system for dual-use orbital delivery.

Be preciseBe uniqueBe Bullet.2019-Present - AdvisorAdvising on engineering and commercial topics.2017-2019 - Lead EngineerRemote and onsite tasks related to the development of the required facilities:. Design and verification of an adaptable ski mold. Design and verification of a pneumatic press frame. Manufacturing of wooden ski mold and steel press frame. Design and assembly of the pneumatic system. Material selection, ski… Show more Be preciseBe uniqueBe Bullet.2019-Present - AdvisorAdvising on engineering and commercial topics.2017-2019 - Lead EngineerRemote and onsite tasks related to the development of the required facilities:. Design and verification of an adaptable ski mold. Design and verification of a pneumatic press frame. Manufacturing of wooden ski mold and steel press frame. Design and assembly of the pneumatic system. Material selection, ski manufacturing, testingBefore 2017Family venture to manufacture skis at home. Show less

Flight Model of a Micro Satellite and a Scalable Hybrid Apogee Kick Rocket Motor:. Mission Systems Engineer. Mechanical Design & Analysis of Scalable Hybrid Rocket Motor. Structural Design & Analysis of the Spacecraft. Configuration. Performance analysis and Motor sizing. Design of Propulsion Feed SystemPreliminary Design of a Hybrid Rocket Motor for a Launcher Upper Stage:. Mechanical Design of the motor. Design of Propulsion Feed System. Performance… Show more Flight Model of a Micro Satellite and a Scalable Hybrid Apogee Kick Rocket Motor:. Mission Systems Engineer. Mechanical Design & Analysis of Scalable Hybrid Rocket Motor. Structural Design & Analysis of the Spacecraft. Configuration. Performance analysis and Motor sizing. Design of Propulsion Feed SystemPreliminary Design of a Hybrid Rocket Motor for a Launcher Upper Stage:. Mechanical Design of the motor. Design of Propulsion Feed System. Performance analysis and Motor sizingConferences:. 2nd Hybrid Rocket Symposium at JAXA/ISAS (Japan), 11-12 July 2019. Presenting themission development, and the micro satellite and Hybrid Rocket Motor flight model designs.. 70th International Astronautical Congress at Washington DC (USA), 21-26 October 2019.Presenting a Hybrid Rocket Motor scalable design for satellite applications. Award: BestTechnical Paper Show less

Head of Mechanical Department, responsible of:. Structural Design and Analysis. Pneumatic Sampling System Design. Configuration of the instrument, Lead Engineer. Components selection (locate vendors). Mass Budget. Assembly and Manufacture. Test. Launch CampaignProject Milestones Attended: Selection, PDR, CDR, progress review, and Launch Campaign.Conferences: . 3rd Symposium on Space Educational Activities, Leicester (UK) 16-18 September 2019… Show more Head of Mechanical Department, responsible of:. Structural Design and Analysis. Pneumatic Sampling System Design. Configuration of the instrument, Lead Engineer. Components selection (locate vendors). Mass Budget. Assembly and Manufacture. Test. Launch CampaignProject Milestones Attended: Selection, PDR, CDR, progress review, and Launch Campaign.Conferences: . 3rd Symposium on Space Educational Activities, Leicester (UK) 16-18 September 2019. Presenting the instrument's innovative design and proof-of-concept goal, as well as the obtained scientific and engineering results.Alternative to AirCore Atmospheric for Greenhouse Gas Sampling (Team Tubular) is a Balloon Experiment for University Students (BEXUS) project, part of the German/Swedish student experiment program REXUS/BEXUS. www.rexusbexus.netProgram Organized by SNSA, DLR, ESA, SSC and ZARM. Show less

At MOST Team at LEGI LabProject: Interactions of two particles in a pipe flow

Project: Catalonia 2030 Strategic Aviation Planning

Hobbie Cat15, RS, Optimist, LaserPico.In charge of english and french clients. Daily and mid-term courses instructor.