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Picosat 9

NSSDCA/COSPAR ID: 2001-043B

Description

Picosat 9 is a British-built (US DOD-funded) microsatellite (67 kg) to test electronic components/systems in space conditions. It carries four test payloads: Polymer Battery Experiment (PBEX), Ionospheric Occultation Experiment (IOX), Coherent Electromagnetic Radio Tomography (CERTO) and an ultra-quiet platform (OPPEX). The name PICO combines the first letters of all four experiments. PICOSat is designed for a minimum of one year of on orbit operations. PICOSat flies in a 800 km circular orbit with a 67 degree inclination. PICOSat uses a gravity gradient boom for stabilization. The body mounted solar panels produce an average on orbit power of 22 W. The Ultra-Quiet Platform (UQP), developed by the Air Force Research Lab, aims to provide a 10:1 reduction in vibration isolation over a 100 Hz bandwidth between the spacecraft bus and a science payload. A PICOSat factsheet can be found at

http://www.losangeles.af.mil/SMC/PA/Fact_Sheets/PICOSat.htm

Alternate Names

  • 26930

Facts in Brief

Launch Date: 2001-09-30
Launch Vehicle: Athena 1
Launch Site: Kodiak Launch Complex, United States

Funding Agency

  • Department of Defense (United States)

Discipline

  • Engineering

Additional Information

Questions or comments about this spacecraft can be directed to: Coordinated Request and User Support Office.

 
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