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EUV Doppler Imaging for CubeSat Platforms

Completed TRL 4 (started at 2, targeting 4)

Description

Provide EUV imaging capability within the resources available for a 3U CubeSat. Advance/extend Extreme Ultraviolet (EUV) imaging capability to small low-cost orbital platforms, providing new capability in the LCAS path for demonstrating EUV instrument concepts that lead to major missions. Develop hardware for first flight demonstration of back-illuminated CMOS active pixel sensors. Demonstrate new Doppler Imaging technique for the EUV.

Mature the design and fabricate the Flare Initiation Doppler Imager (FIDI) instrument to demonstrate low-spacecraft-resource EUV technology (most notably, back-illuminated CMOS) from a 3U CubeSat platform, using a recently-developed EUV Doppler imaging technique (see upper right panel).

Benefits

FIDI will provide doppler shift measurements of a line observed by SDO/AIA

Details

Technology areaSensors and Instruments > Observatories
ProgramCenter Independent Research & Development: GSFC IRAD (GSFC IRAD)
Lead organizationGoddard Space Flight Center, Greenbelt, MD
Start date2011-10-01
End date2012-09-30

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