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[[File:Uwe2-in-cleanroom.JPG|thumb|left|alt= UWE-2 im Reinraum]]
[[File:Uwe2-in-cleanroom.JPG|thumb|left|alt= UWE-2 im Reinraum]]
*[http://www7.informatik.uni-wuerzburg.de/en/research/research_groups/space_exploration/projects/cubesat/uwe_2/ UWE-2 homepage]
*[https://web.archive.org/web/20110719111413/http://www7.informatik.uni-wuerzburg.de/en/research/research_groups/space_exploration/projects/cubesat/uwe_2/ UWE-2 homepage]
*[http://idw-online.de/pages/de/news335222 Uni-Satellit UWE-2 erfolgreich gestartet], Gunnar Bartsch, Stabsstelle Öffentlichkeitsarbeit, Julius-Maximilians-Universität Würzburg, 23 September 2009.
*[http://idw-online.de/pages/de/news335222 Uni-Satellit UWE-2 erfolgreich gestartet], Gunnar Bartsch, Stabsstelle Öffentlichkeitsarbeit, Julius-Maximilians-Universität Würzburg, 23 September 2009.
*[http://www7.informatik.uni-wuerzburg.de/en/research/research_groups/space_exploration/projects/cubesat/uwe_3/ information on UWE-3]
*[https://web.archive.org/web/20110719111700/http://www7.informatik.uni-wuerzburg.de/en/research/research_groups/space_exploration/projects/cubesat/uwe_3/ information on UWE-3]


{{Orbital launches in 2009}}
{{Orbital launches in 2009}}

Revision as of 09:55, 11 November 2017

UWE-2
OperatorUniversity of Würzburg
COSPAR ID2009-051D Edit this at Wikidata
SATCAT no.35934Edit this on Wikidata
Spacecraft properties
Launch mass< 10 kilograms (22 lb)
Start of mission
Launch date23 September 2009, 06:21 (2009-09-23UTC06:21Z) UTC
RocketPSLV C14
Launch siteSatish Dhawan FLP
Orbital parameters
Reference systemGeocentric

The University Würzburg's Experimental satellite 2 (UWE-2) is a CubeSat of a length of 10 cm and a mass of 1 kg. Developed by the University of Würzburg, its scientific objectives are;

  • tests of methods and algorithms for attitude determination,
  • optimisation of internet protocol parameters, in order to adapt to the specific space environment.

On 23.9.2009 UWE-2 was launched by an Indian PSLV rocket (PSLV-C14) together with Oceansat-2 and three further CubeSats in a polar orbit at 730 km altitude. Successful operations could be initiated.

UWE-2 followed the earlier UWE-1. UWE-3 is also planned.

See also

UWE-2 im Reinraum