Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Jaan Viru"'
Autor:
Andris Slavinskis, Mario F. Palos, Janis Dalbins, Pekka Janhunen, Martin Tajmar, Nickolay Ivchenko, Agnes Rohtsalu, Aldo Micciani, Nicola Orsini, Karl Mattias Moor, Sergei Kuzmin, Marcis Bleiders, Marcis Donerblics, Ikechukwu Ofodile, Johan Kütt, Tõnis Eenmäe, Viljo Allik, Jaan Viru, Pätris Halapuu, Katriin Kristmann, Janis Sate, Endija Briede, Marius Anger, Katarina Aas, Gustavs Plonis, Hans Teras, Kristo Allaje, Andris Vaivads, Lorenzo Niccolai, Marco Bassetto, Giovanni Mengali, Petri Toivanen, Iaroslav Iakubivskyi, Mihkel Pajusalu, Antti Tamm
Publikováno v:
Aerospace, Vol 11, Iss 3, p 230 (2024)
The electric solar wind sail, or E-sail, is a propellantless interplanetary propulsion system concept. By deflecting solar wind particles off their original course, it can generate a propulsive effect with nothing more than an electric charge. The hi
Externí odkaz:
https://doaj.org/article/dda7df98fcc8422db0ad077d1eb22aa6
Autor:
Petri Toivanen, Johan Kutt, Jaanus Kalde, Roland Rosta, Mihkel Pajusalu, Mart Noorma, Paul Liias, Andris Slavinskis, S. Lätt, Jouni Polkko, Hendrik Ehrpais, Jouni Envall, Karoli Kahn, Tõnis Eenmäe, Erik Kulu, Taneli Kalvas, Indrek Sünter, Riho Vendt, Pekka Janhunen, Urmas Kvell, Henri Kuuste, Karlis Zalite, Erik Ilbis, Viljo Allik, Kaspars Laizans, Jaan Viru
Publikováno v:
IEEE Aerospace and Electronic Systems Magazine. 30:12-22
ESTCube-1 is a student satellite project lead by the University of Tartu, Estonia, and supported by the European Space Agency (ESA) via Plan for European Cooperating States (PECS). Development of ESTCube-1 has been a collaborative effort with many in
Autor:
Johan Kutt, Andris Slavinskis, Jaan Viru, Erik Kulu, Mart Noorma, Indrek Sünter, Henri Kuuste, Hendrik Ehrpais
Publikováno v:
Journal of Aerospace Engineering. 29
This paper presents the characterization and in-orbit validation of the ESTCube-1 attitude determination system (ADS). ESTCube-1 is a one-unit CubeSat built by students and launched on May 7, 2013, to a Sun-synchronous, 700-km, polar low Earth orbit.
Autor:
Erik Kulu, Kaspars Laizans, Jouni Envall, R. Valner, Viljo Allik, Kaupo Voormansik, E. Soolo, Ilmar Ansko, M. Järve, T. Uiboupin, Urmas Kvell, Jaan Viru, Henri Kuuste, Indrek Sünter, T. Scheffler, Erik Ilbis, Mart Noorma, Tõnis Eenmäe, S. Lätt, Riho Vendt, Andris Slavinskis, Jaanus Kalde, Hendrik Ehrpais
Publikováno v:
Proceedings of the Estonian Academy of Sciences. 63:242
This paper presents the design, development, and pre-launch characterization of the ESTCube-1 Attitude Determination and Control System (ADCS). The design driver for the ADCS has been the mission requirement to spin up the satellite to 360 deg¢s i1