From the IARU Amateur Satellite Frequency Coordination pages at 
http://www.amsat.org.uk/iaru/formal_detail.asp?serial=168 

POPACS-RR a 2U cubesat will use self-contained, warm gas, propulsion system to 
adjust satellite’s initial circular orbit of 450 km to eccentric orbit with 
apogee of 1500 km and perigee of 450 km. Demonstrate use of 3D printing (a.k.a. 
rapid prototyping) for manufacturing small satellites. Measure flux of 
energetic particles in lower Van Allen Belt. Test radiation-hardened electronic 
components and high performance solar cells in high radiation environment over 
a period of five years. Test radiation hardened components for a Plug and Play 
satellite. Proposing a UHF downlink of 9k6 GMSK AX25 packet and also an S Band 
downlink of BPSK at 9k6 or 38k4. Planning a launch on the first flight of 
SpaceX Falcon 1E not earlier than May 2011 with a 45 deg inclination. Will 
apply for a FCC part 5 Experimental licence for this project.

IARU Amateur Satellite Frequency Coordination pages 
http://www.amsat.org.uk/iaru/

73 Trevor M5AKA
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