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Terra Launch - December 18, 1999 |
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Installation of flight multi-layer insulation on CERES Flight Models
1 and 2 at the TRW clean room facility after completion of calibration
in preparation for shipment to Vandenberg for integration on Terra.
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Installation of protective MLI blanket cover on the DAA power converter assembly |
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Exterior of CERES sensor assembly. Three such sensors (total,
shortwave, and window channels) are installed in each CERES instrument.
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Cutaway of CERES sensor assembly showing heat-sink disk on the left
with the active detector flake mounted to it, field stop and telescope
baffle to the right.
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'Family portrait' showing the ERBE Engineering Model and the CERES
PFM, FM1, and FM2 which fly on TRMM and Terra. ERBE scanners flew on
ERBS, NOAA-9 and NOAA-10 from 1984 to 1990.
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Illustration of the planned scanning operations for the two CERES
instruments. The CERES FORE (FM1) instrument, shown on the right side
of the picture, is scanning the earth in a nominal crosstrack configuration.
The CERES AFT (FM2) instrument, shown on the left side of the picture, is
scanning the earth in a nominal biaxial configuration |
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CERES instruments mounted on the Terra spacecraft during integration
and testing. Image shows instruments with main and mam contamination
covers in their closed and opened positions.
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