| Organization | NASA |
|---|---|
| Major Contractors | Lockheed Martin |
| Mission Type | Earth Observation |
| Satellite of | Earth |
| Launch | September 15, 1991 from Space Shuttle |
| Mission Duration | September 15, 1991–December 15, 2005 |
| Mass | 5,900 kg |
| Webpage | http://umpgal.gsfc.nasa.gov/ |
| Orbital elements | |
| Semimajor Axis | 600 lm |
| Inclination | 57° |
| Orbital Period | 95.9 minutes |
| Instruments | |
| Cryogenic Limb Array Etalon Spectrometer (CLAES) | Determines concentrations and distributions of gasses in atmosphere |
| Improved Stratospheric and Mesospheric Sounder (ISAMS) | Creates a temperature profile of the middle atmosphere |
| Microwave Limb Sounder (MLS) | Create vertical profiles of atmospheric gasses, temperature, pressure and cloud ice |
| Halogen Occultation Experiment (HALOE) | Profile the middle atmosphere composition and temperature |
| High Resolution Doppler Imager (HRDI) | Uses Doppler shift to determine horizontal winds |
| Wind Imaging Interferometer (WINDII) | Senses temperature and winds in the mesosphere and lower thermosphere |
| Solar Ultraviolet Spectral Irradiance Monitor (SUSIM) | Measures the absolute irradiance of the solar ultraviolet (UV) light |
| Solar/Stellar Irradiance Comparison Experiment (SOLSTICE) | (characteristics) |
| Particle Environment Monitor (PEM) | (characteristics) |
| Active Cavity Radiometer Irradiance Monitor (ACRIM II) | (characteristics) |
The Upper Atmosphere Research Satellite (UARS) is an orbital observatory whose mission is to study the Earth’s atmosphere, particularly the protective ozone layer.
The 5900 kg (13,000 lb) satellite was launched during Space Shuttle mission STS-48 in 1991. The original mission life was to be three years. As of June of 2005, six of the ten instruments were still operational. UARS orbits at an altitude of 375 miles with an orbital inclination of 57 degrees.
A final orbit lowering burn, followed by the "passivation" of the Satellite's systems was performed in early December, 2005.
In order to differentiate the relatively weak signature of trace gases from the background radiation in the atmosphere, CLAES had to have high resolution and sensitivity. To achieve this, the instrument combined a telescope with an infrared spectrometer. The whole instrument was cryogenically cooled to keep heat from the instrument from interfering with the readings. The cryogenics system consists of an inner tank of solid neon at −257 °C (−430 °F) and an outer tank of solid carbon dioxide at −150 °C (−238 °F). As the neon and carbon dioxide evaporated, they kept the instrument cool. The final cryogens evaporated from the instrument on May 5, 1993 and the instrument warmed up ending its useful life.
The instrument looked sideways out of the UARS platform to allow the instrument to look through the stratosphere and the lower mesosphere. CLAES produced a 19-month global database showing the vertical distributions of important ozone-layer gases in the stratosphere and their variation with time of day, season, latitude, and longitude.
Thermal radiation enters the instrument through a three-mirror antenna system. The antenna mechanically scans in the vertical plane through the atmospheric limb every 65.5 seconds. The scan covers a height range from the surface up to 90 km (55 miles). Upon entering the instrument, the signal from the antenna is separated into three signals for processing by different radiometers. The 63-GHz radiometer measures temperature and pressure. The 183-GHz radiometer measures water vapor and ozone. The 205-GHz radiometer measures ClO, ozone, sulfur dioxide, nitric acid and water vapor.
As of June 2005, the 63- and 205-GHz radiometers are operational. The 183-GHz radiometer failed after 19 months of operation.
A vertical scan of the atmosphere is obtained by tracking the sun during occultation. The scan will measure the amount of solar energy absorbed by gasses in the atmosphere.
In order to support scanning, the instrument comes in two parts, the optics unit on a two-axis gimbal and a fixed electronics unit. The optics unit contains a telescope that collects solar energy as well as the gas detectors. The electronics unit handles data, motor control and power for the instrument.
The instrument consists of two parts, the telescope and the interferometer which consists of an optical bench and support electronics.
The telesope uses a narrow field of view to prevent Doppler shift variation across the field of view from distorting the results. Input from the telescope is fed to the processor via a fiber optic cable.
HRDI has been turned off since April 17, 1995 due to a problem with the spacecraft’s solar array.
The instument consists of an interferometer which feeds to a CCD camera. The two telescopes (45 degrees and 135 degrees) each have a one meter long baffle tube to reduce stray light during daytime viewing. The input from the telescopes is positioned side-by-side on the CCD so both views are imaged simultaneously.
Because of the energy of UV, instrument degradation is a major issue. To help with this problem, the instrument contains two identical spectrometers. One will is used almost continuously during the daylight portion of UARS’ orbit. The second is used infrequently to verify the sensitivity of the first.
This article is licensed under the GNU Free Documentation License.
It uses material from the
"Upper Atmosphere Research Satellite".
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