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Demosat 2



General


Designation 28500 / 04050A
Launch date 21 Dec 2004
Country of origin United States
Mission Experimental
Perigee/Apogee 19401/36420 km
Inclination 13.5°
Period 1045 min
Launch vehicle Delta 4 Heavy

Demosat 2 was to be released into a 36,340 km x 36,342 km x 10 degrees orbit after a 5 hours, 14 minutes coast period and a third ignition of the upper stage.

sat-index articles


Technical data



Specifications


Prime contractor  
Platform  
Mass at launch 6020 kg
Mass in orbit  
Dimension 1.38 m diameter, 1.95 m high
Solar array  
Stabilization  
DC power  
Design lifetime  

The outer skin is an aluminium structure, with inner ballast consisting of sixty 11.4 cm diameter brass rods. Stiffeners, plates, fasteners and fittings complete the payload.

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