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Polysat CP4

CalPoly 4, an exact replica of Polysat CP2


Designation 31132 / 07012Q
Launch date 17 Apr 2007
Country of origin United States
Mission Technology
Perigee/Apogee 646/793 km
Inclination 98°
Period 99 min
Launch vehicle Dnepr #8

Built by California Polytech. The primary mission of CP3 is to implement an attitude control system using only magnetic torquers embedded within the side panels.

1 kg, downlink 437.325 MHz

CP 2 was destroyed in the Jul 2006 Dnepr launch failure.

External resources


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