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DTUsat



General


Designation 27842 / 03031C
Launch date 30 Jun 2003
Country of origin Denmark
Mission Technology
Perigee/Apogee 820 km, sunsynchronous
Inclination  
Period  
Launch vehicle Rokot #9

Operated by the Technical University of Denmark

Carries a 450 m tether.

External resources


http://www.dtusat.dtu.dk/

sat-index articles


Technical data



Specifications


Prime contractor  
Platform  
Mass at launch 1 kg
Mass in orbit  
Dimension  
Solar array  
Stabilization  
DC power  
Design lifetime  

Downlink: 437.475 MHz FM AFSK 2400 bps

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