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  • Lessons learned from three university experiments onboard the REXUS/BEXUS sounding rockets and stratospheric balloons

    Paper number

    IAC-13,D1,5,3,x18413

    Author

    Mr. Thomas Sinn, University of Strathclyde/Advanced Space Concepts Laboratory, United Kingdom

    Coauthor

    Mr. Malcolm McRobb, University of Glasgow, United Kingdom

    Coauthor

    Mr. Roy Brown, Electronic & Electrical Engineering / University of Strathclyde, United Kingdom

    Coauthor

    Mr. Adam Wujek, Royal Inst. of Technology (KTH), Sweden

    Coauthor

    Mr. Christopher Lowe, University of Strathclyde/Advanced Space Concept Laboratory, United Kingdom

    Coauthor

    Mr. Johannes Weppler, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany

    Coauthor

    Mr. Thomas Parry, University of Strathclyde, United Kingdom

    Coauthor

    Mr. Daniel García Yárnoz, University of Strathclyde/Advanced Space Concept Laboratory, United Kingdom

    Coauthor

    Mr. Frazer Brownlie, University of Strathclyde / Mechanical and Aerospace Engineering, United Kingdom

    Coauthor

    Mr. Iain Dolan, United Kingdom

    Coauthor

    Mr. Tiago de Franca Queiroz, University of Strathclyde / Computer Science, United Kingdom

    Coauthor

    Mr. Fredrik Rogberg, KTH Mechanics, Royal Institute of Technology, Sweden

    Coauthor

    Mr. Nathan Donaldson, University of Strathclyde, United Kingdom

    Coauthor

    Mr. Ruaridh Clark, United Kingdom

    Coauthor

    Dr. Gunnar Tibert, Royal Institute of Technology (KTU), Sweden

    Year

    2013

    Abstract
    Since the start of my PhD in October 2010, I was involved in three experiments that were or will be launched on sounding rockets and high altitude balloons with the REXUS/BEXUS program (Rocket-bourne / Balloon-bourne Experiments for University Students). The REXUS BEXUS program is organised and sponsored by the German Aerospace Center (DLR), the Swedish National Space Board (SNSB) and the European Space Agency (ESA). The first experiment, called Suaineadh was launched from Esrange (Kiruna, Sweden) onboard REXUS 12 in March 2012. Suaineadh had the purpose of deploying a web in space by using centrifugal forces. Unfortunately, the payload was lost during re-entry and a recovery mission to Kiruna in North Sweden was undertaken. StrathSat-R is the second experiment which will deploy two cube satellites with inflatable structures from the REXUS 13 sounding rocket after launch in May 2013. The last experiment is the iSEDE experiment which has the goal of deploying an inflatable structure with disaggregated electronics from the high altitude balloon BEXUS15/16 in September 2013. All these experiments are designed, built and flown in a timeframe of one and a half to two years, kicking off with experiment proposals every October (2010, 2011 and 2012). This paper will present the lessons learned in project management, outreach, experiment design, fabrication and manufacturing, software design and implementation, testing and validation as well as launch, flight and post-flight. Furthermore, the lessons learned during the recovery mission of Suaineadh will be discussed as well. All these experiments were designed, build and tested by a large group of university students of various disciplines and different nationalities. StrathSat-R and iSEDE were build completely in Strathclyde but the Suaineadh experiment was a joint effort between Glasgow and Stockholm which was especially tricky during integration while approaching the experiment delivery deadline. This paper should help students and professionals across various disciplines to build and organise these kinds of projects more efficiently without making the same, sometimes expensive, mistakes all over again.
    Abstract document

    IAC-13,D1,5,3,x18413.brief.pdf

    Manuscript document

    IAC-13,D1,5,3,x18413.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.