000022840 001__ 22840
000022840 005__ 20220110134529.0
000022840 04107 $$aeng
000022840 046__ $$k2018-05-14
000022840 100__ $$aOstaszewski, M.
000022840 24500 $$aCanSat mini-satellite project. Test procedure and mission implementation

000022840 24630 $$n24.$$pEngineering Mechanics 2018
000022840 260__ $$bInstitute of Theoretical and Applied Mechanics of the Cech Academy of Sciences, Prague
000022840 506__ $$arestricted
000022840 520__ $$2eng$$aThe only limitation for human curiosity is our technological advancement. History has thought us that space exploration is one of the most significant driving force of human development. One of the means to explore the universe are artificial satellites. They can perform tasks unachievable for us. Construction of the satellite is very complicated and time-consuming process. Fortunately, several classes of satellites are distinguished. Entry level one- CanSat has similar dimensions to an ordinary soda can. The main subject of this paper is the construction of these type of satellites. Then all testing procedure and every part of the mission is described. At the end of the paper conclusions and suggestions for further development are expressed.

000022840 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000022840 653__ $$aminisatellite, CanSat, rocket

000022840 7112_ $$aEngineering Mechanics 2018$$cSvratka, CZ$$d2018-05-14 / 2018-05-17$$gEM2018
000022840 720__ $$aOstaszewski, M.$$iDzierżek, K.
000022840 8560_ $$ffischerc@itam.cas.cz
000022840 8564_ $$s441611$$uhttps://invenio.itam.cas.cz/record/22840/files/629.pdf$$yOriginal version of the author's contribution in proceedings, page , section MCT.
000022840 962__ $$r21225
000022840 980__ $$aPAPER