Zobrazeno 1 - 10
of 39
pro vyhledávání: '"Palmer, Kristoffer"'
Autor:
Palmer, Kristoffer
In this thesis, components intended for vehicles in space and other extreme environments have been realized using microsystems technology to facilitate miniaturized, yet high-performing systems beneficial for small spacecraft and other vehicles with
Externí odkaz:
http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-186862
Publikováno v:
In Propulsion and Power Research September 2020 9(3):216-224
Autor:
Sjöholm, Johan, Palmer, Kristoffer
Publikováno v:
ISSN 1401-5757 (2007)
In this diploma thesis we study the characteristics of electromagnetic fields carrying orbital angular momentum (OAM) by analyzing and utilizing results achieved in optics and then apply them to the radio domain to enable innovative radio studies of
Externí odkaz:
http://arxiv.org/abs/0905.0190
Publikováno v:
In Sensors & Actuators: A. Physical 15 October 2013 201:49-57
Autor:
Jonsson, Jonas, Sundqvist, Johan, Nguyen, Hugo, Berglund, Martin, Ogden, Sam, Palmer, Kristoffer, Smedfors, Katarina, Johansson, Linda, Hjort, Klas, Thornell, Greger
Publikováno v:
In Acta Astronautica October-November 2012 79:203-211
Publikováno v:
Small Satellite Conference
Cubesats is rapidly maturing beyond educational projects and low cost technology demonstrators. Today we want cubesats to provide useful data with a scientific or commercial value. One of the unique advantages of cubesats is that the size and cost en
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1459::e2d97edffd4fc6c79977487416b1dda1
https://digitalcommons.usu.edu/smallsat/2016/S6Propulsion/1
https://digitalcommons.usu.edu/smallsat/2016/S6Propulsion/1
Akademický článek
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Autor:
Rangsten, Pelle, Palmer, Kristoffer, Bejhed, Johan, Zaldivar Salaverri, Ana, Jonsson, Kerstin, Grönland, Tor-Arne
Publikováno v:
AIAA/USU Conference on Small Satellites
This paper presents a MEMS-based micro propulsion system with closed-loop thrust control. It is a cold gas system with butane as propellant packaged in module with the size one third of a 1U CubeSat. The module is described in terms of design, manufa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1459::20e5be4bce5db2013ccc9af74f903fd7
http://digitalcommons.usu.edu/smallsat/2013/all2013/100
http://digitalcommons.usu.edu/smallsat/2013/all2013/100
For aggressive environments, the material properties of silicon become a limitation. Macroscopically, ceramics are as common for high-temperature applications as is silicon in miniaturized systems, but this group of materials has been little exploite
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::c502e5355037523fa8923d87a46ceb6e
http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-164386
http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-164386