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REXUS 6
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REXUS 6

REXUS

Rocket-borne Experiments for University Students

REXUS 6 was successfully launched from Esrange Space Center on March 12, 2009 at 10.08 UTC. 
The rocket reached an apogee of approximately 88,4 km.

Download the video of the launch from DLR's website: 
http://www.dlr.de/rd/desktopdefault.aspx/tabid-5305/8894_read-16381/

GENERAL INFORMATION

Launch site: Esrange Space Center
Launch date: 12 March, 2009 at 10:08 UTC
Customer: The REXUS program is a joint project between the Swedish Space Corporation SSC, ESRANGE, and the Mobile Rocket Base (Moraba) of the German Aerospace Center DLR, conducted by EUROLAUNCH. Half of the payload is reserved for German students, while the Swedish half has been made available to students from other European countries through a collaboration with ESA Education. REXUS is considered as an annual sounding rocket program, launched from Esrange Space Center, Sweden.
Media information Press releases, photos and/or videos are found here. Read more about Rexus programme here.

TECHNICAL INFORMATION
Rocket type: One stage solid, Improved Orion rocket
Nominal diameter: 356 mm
Lenght: ca 5600 mm
Total weight: 517,7 kg
Burning time 1st stage: 26 s
Max acceleration: 21 g

Apogee:

~100 km
Flight time to apogee: ~150 sec

EXPERIMENT MODULES

Rexus-6_payload

  • AGADE - Applied Geomagnetics for Attitude Determination Experiment.
    The Applied Geomagnetics for Attitude Determination Experiment aims for analysing and comparing a set of different of-the-shelf small 3-axes magnetometer assemblies. These are going to be launched together with a high precession magnetometer. For further analysis time-dependant variations of earth's magnetic field will be registered on the ground. After the the flight, the resulting data will be used for evaluating advanced on-board attitude determination software for the future SOMP cubesat.
     
    Team:
    Sebastian M. Ernst (Freiberg University of Mining and Technology, Germany)
    Martin Laabs (Dresden University of Technology, Germany)
    Stefan Golla (Brandenburg University of Technology, Germany)
    Hannes Weisbach (Dresden University of Technology, Germany)
    Stefan Oettel (Dresden University of Technology, Germany)
    Marian Hillemann (Dresden University of Applied Science, Germany)
    Erik Winkelmann (Dresden University of Applied Science, Germany)
    Georg Bauerfeind (Dresden University of Applied Science, Germany)

  • NISSE - Nordic Ionospheric Sounding Rocket Seeding Experiment.
    In the NISSE experiment 19 kg of water will be released into the ionosphere at an altitude of about 95 km. Fifth of the water is expected to flash evaporate in the low pressure atmosphere immediately when released. The cooling of evaporation may first cause the rest of the water to turn into ice, which will sublimate in the order of seconds to minutes, depending on the crystal size. The vapour cools down while expanding into the surrounding space. The molecules may condensate to a cloud of tiny ice crystals due to the abrupt temperature drop caused by adiabatic cooling by expansion. Then the ice particles will re-evaporate back into a gaseous stage when reaching the temperature of the background atmosphere. The water molecules will be ionized by solar radiation and ion chemistry, modifying the ambient ion composition in the cloud.
     
    The tristatic EISCAT UHF incoherent scatter radar system located in the Northern Scandinavia, in Tromsø, Norway, Kiruna, Sweden and Sodankylä, Finland will be used in the detection of the water release. The changes in the ion composition will cause local variations in the ionospheric plasma parameters, e.g. electron density variations, that can be measured by the UHF radar. The water release will be attempted to detect by the UHF radar to study its behaviour under prevailing lowthermospheric neutral wind and electric and magnetic field conditions. In addition, the effect of the release to the incoherent scatter spectrum will be investigated.
     
    Besides the standard EISCAT data processing, the UHF raw data during the experiment is planned to be sampled in collaboration with the Sodankylä Geophysical Observatory, Finland, enabling sophisticated additional post-experiment analysis using statistical inversion methods.
     
    Team:
    Vidar Hølland (University of Bergen, Norway)
    Gard Mellemstrand (NTNU, Norway)
    Timo Pitkänen (University of Oulu, Finland)
    Gisela Baumann (University of Helsinki, Finland)

Contact persons:
Olle Persson, EuroLaunch (SSC Esrange), olle.persson@ssc.se
Andreas Stamminger, EuroLaunch (DLR Institute of Space Systems), andreas.stamminger@dlr.de

Read more about REXUS at the REXUS/BEXUS website: www.rexusbexus.net
ESAs website for REXUS and BEXUS: http://www.esa.int/SPECIALS/Education/SEMTTQJV3AF_0.html



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