
The MR beacon CW power is plotted versus time in this figure. The gain in
our direction during the normal 100-minute spacecraft spin was at maximum
just before 16:00 UTC on November 25, 1996. The spacecraft began instrument
calibrations at 16:18 (16.3 hours in the figure) and the calibrations
continued through 17:40 (17.7 hours). During this time, the MOC camera was
swept first past the Earth and then the Moon. The MR gain in our direction
was again quite large at these times. This figure was obtained using our
low-volume archive of thresholded data and should be considered preliminary.

The MR beacon frequency is plotted versus time above. The frequency of
the peak signal in each of our spectra is indicated with a '+'. Post
processing will allow us to better estimate the received MR beacon
frequency as a function of time. The frequency changes smoothly with time
due primarily to Doppler shifts caused by the Earth's rotation. This figure
was obtained using our low-volume archive of thresholded data and
should be considered preliminary. Our frequency resolution for the
processing of the MR beacon signal was approximately 7.5 Hertz.
Last updated: 02 December 1996
Joe Twicken