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The 2232 kg (4919
lbm) satellite is the latest in the series of advanced TIROS-N
spacecraft that provide a platform to support the environmental
monitoring instruments for imaging and measuring the Earth's
atmosphere, its surface and cloud cover. The spacecraft is the
second in a series of five Polar Operational Environmental
Satellites (POES) to be built by Lockheed Martin Space Systems
Company, Sunnyvale, CA. The operational system consists of two
polar-orbiting satellites. The polar-orbiting spacecraft serve as
complementary satellites to the geosynchronous Geostationary
Operational Environmental Satellites (GOES) system. NOAA M also
provides a platform for the Search and Rescue Satellite Aided
Tracking system, part of the COSPAS-SARSAT constellation. The
Search and Rescue satellites (SARSAT/COSPAR) have been
instrumental in saving more than 13,000 lives since the inception
of the system.
The instruments
onboard the satellite include the Advanced Very High Resolution
Radiometer (AVHRR/3), the High Resolution Infrared Radiation
Sounder (HIRS/3), the Advanced Microwave Sounding Unit-A (AMSU-A1,
A2), the AMSU-B, the Solar Backscatter Ultraviolet Radiometer
(SBUV/2), the Space Environment Monitor (SEM/2) and the Data
Collection System (DCS/2). The AVHRR/3 is the primary imaging
system, which consists of visible, near infrared (IR) and thermal
IR channels. The primary sounding suite is the HIRS/3, AMSU-A and
AMSU-B, which measures atmospheric temperature and humidity. The
SBUV/2 instrument is both an imager and a sounder. As an imager,
it produces total column ozone maps. As a sounder, it obtains and
measures the ozone distribution in the atmosphere as a function of
altitude.
In addition to
the weather instruments, the satellite carries two search and
rescue instruments, the Search and Rescue Repeater (SARR) and the
Search and Rescue Processor (SARP).

NOAA
POES 17 (M)
National
Oceanic
and Atmospheric
Administration
Polar
Operational
Environmental
Satellite
|
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SPACECRAFT
|
| Int'l Designation |
2002 032A
|
Launched
|
| Owner / Sponsor |
U.S.
National Oceanic and Atmospheric Administration (NOAA)
|
| Mission |
Weather
observation
|
| Manufacturer |
Lockheed
Martin
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|
| Launch Mass |
2232
kg (4919 lbm)
|
| Dimensions, stowed |
|
| Mission Orbit |
LEO
-
833 km (450 nmi)
|
98.7465°
|
| Design Life |
2
years
|
| Power (EOL) |
|
| Other names |
NOAA
M
|
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LAUNCH
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| Launch Vehicle
Model |
Titan
II |
| Date / Time (UTC) |
24
June 2002
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18:23:03.656
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|
FINANCIAL
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| Satellite cost |
US$202
million
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| Web Links |
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