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NASA NTRS · 20190025500

SMAP Instrument Antenna, on Orbit Performance Validation and Verification

Focardi, Paolo·Spencer, Michael W.·Piepmeier , Jeffery R
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Abstract

NASA’s Soil Moisture Active Passive (SMAP) Mission is currently flying in a 685 km orbit. Featuring a Synthetic Aperture Radar (SAR) and a radiometer sharing the same antenna, SMAP was developed in collaboration between Jet Propulsion Laboratory (JPL) and Goddard Space Flight Center (GSFC). While the radar requirements on the instrument antenna were more benign from an RF point of view, the radiometer requirement were more difficult to meet because of the stability required by the radiometer to operate to its full potential. The instrument antenna performance was predicted by a very detailed RF model and verified by measuring a 1/10th scale model with great accuracy before launch. Once in orbit, we had the opportunity to measure the antenna performance for both the radiometer and the radar and compare it with the predicted performance given by our RF model. This paper discusses the work done both at JPL and GSFC in order to verify and validate the on orbit performance of the SMAP instrument antenna.

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Focardi, Paolo, Spencer, Michael W., Piepmeier , Jeffery R. 2016-06-26. SMAP Instrument Antenna, on Orbit Performance Validation and Verification. https://ntrs.nasa.gov/citations/20190025500

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