cancel
 
 

CERES Logo
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

CERES Brochure


Image: First Page Image: Previous Page Image: Next Page Image: Last Page

CERES Instrument

CERES instrument assembly Image

CERES instrument assembly (TRW)

The CERES instrument pictured on the right is based on the successful ERBE scanning radiometer design with several improvements to accommodate upgraded performance requirements and hardware developments. CERES has twice the spatial resolution and improved instrument calibration. The two EOS spacecrafts will each carry two identical instruments: one will operate in a cross-track scan mode and the other in a biaxial scan mode. The cross-track scan will essentially continue the measurements of the ERBE, while the biaxial scan mode will provide new angular flux information that will improve the accuracy of angular models used to derive the Earth's radiation balance.

Each CERES instrument has three channels -- a shortwave channel to measure reflected sunlight, a longwave channel to measure Earth-emitted thermal radiation in the 8-12 μm "window" region, and a total channel to measure all wavelengths of radiation. Onboard calibration sources include a solar diffuser, a tungsten lamp system with a stability monitor, and a pair of blackbodies that can be controlled at different temperatures. Cold space looks and internal calibration are performed during normal Earth scans. During the first year of operation on TRMM, CERES has shown remarkable stability. There has been no discernable change in instrument gain for any channel at the 0.2% level with 95% confidence. Ground and in-space calibrations agree to within 0.25%.


Technical Specifications


Orbits 705 km altitude, 10:30 a.m. descending node (Terra) or
1:30 p.m. ascending node (PM-1), sun-synchronous, near-polar;
350 km altitude, 35o inclination (TRMM)
Spectral Channels Solar Reflected Radiation (Shortwave): 0.3 - 5.0 μm
Window: 8 - 12 μm
Total: 0.3 to > 100 μm
Swath DimensionsLimb to limb
Angular SamplingCross-track scan and 360o azimuth biaxial scan
Spatial Resolution20 km at nadir (10 km for TRMM)
Mass45 kg
Duty Cycle100%
Power45 W
Data Rate10 kbps
Size60 x 60 x 70 cm (deployed)
Design Life6 years

The CERES instrument is managed by the NASA Langley Research Center in Hampton, Virginia, and built by TRW's Space and Technology Group in Redondo Beach, California.



Image: First Page Image: Previous Page Image: Next Page Image: Last Page
12

 
 
 
Page Curator: Joanne Saunders
NASA Official: Dr. Norman Loeb
Page Last Modified: 05/16/2014 14:29
+ Privacy Policy and Important Notices
+ USA.gov
+ ExpectMore.gov
+ Multimedia Browser Plug-ins
+ Comments or Questions?