Thermal Mapping Channel Spectral Response

The end-to-end spectral response of the Diviner flight instrument has been determined. Representative response curves for the four Diviner thermal mapping channels are shown at right.

Mineralogy Channel Spectral Response

The end-to-end spectral response of the Diviner flight instrument has been determined. Representative response curves for the three Diviner mineralogy mapping channels are shown at right.

Signal To Noise Ratio

The signal to noise ratio of the Diviner flight instrument has been characterized. Representative Noise Equivalent Temperature Delta (NETD) curves for Diviner's four thermal mapping channels are shown at right. Diviner's minimum detectable temperature is in the neighborhood of 30K.



The Diviner Lunar Radiometer Experiment is funded by NASA through the Lunar Reconnaissance Orbiter Project at NASA Goddard.
The instrument is built and operated by JPL.

Contact Us