This paper presents radiation dosimetry results from the radiation and
reliability assurance experiments on the Clementine spacecraft and In
terstage Adapter Satellite. The dosimetry instruments utilize low-dose
-response p-channel field-effect-transistor and proton-sensitive stati
c-RAM dosimeters. These dosimeters successfully demonstrated an order-
of-magnitude decrease in instrument weight and power from previous sys
tems. The data confirm prelaunch predictions of the total-dose effects
on charge-coupled-device dark current and on complementary-metal-oxid
e-semiconductor 1.2 and 0.8-mu m technology design and process paramet
ers in the space environment. A solar proton event during the early ph
ases of the mission allowed a comparison between the Clementine measur
ed proton fluence and energy spectra and the Geostationary Operational
Environmental Satellite 6 measured proton fluence and energy spectra.
These data confirmed the proton-spectrometer design and operation.