A long-running polar orbit weather satellite constellation serving the troops of the United States will receive its newest member soon with the launch of a fresh satellite. The United States Air Force’s Defense Meteorological Satellite Program (DMSP), once a national top-secret program, will refresh its constellation with the launch of DMSP F19, slated to be its 2nd-to-last satellite to be launched into orbit. With a suite of meteorological instruments similar to those working on NOAA's polar weather satellite fleet (latest being the NPP), it provides detailed weather information to USAF (and to a certain extent civilian) meteorologists to provide long term weather forecasting data for tactical planning.
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Viewing the Launch Live:
Mission Description:
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Launch preparations photos:
Launch Updates:
Launch Vehicle:
Launch Timeline & Ground Track:
Weather Forecast for Vandenberg AFB, California on April 3, 2014 (8 a.m.)
Partly to mostly cloudy. High near 16C. Winds W at 15 to 25 kmh.
Time|Temps|Dew Point|Relative Humidity|Precip|Snow|Cloud cover|Pressure|Wind|Weather
6 AM|8°C|6°C|87%|0%|0%|6%|1018 hPa|6 km/h E|
Clear
Links:
![](https://upload.wikimedia.org/wikipedia/en/thumb/b/b2/ULA_logo.svg/220px-ULA_logo.svg.png)
Launch date:
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April 3, 2014
Launch time:
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14:46-14:56 UTC / 7:46-7:56 a.m. PDT / 10:46-10:56 a.m. EDT
Launch site:
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SLC-3E, VAFB, California
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[highlight]L[eventtimer]2014-04-03 14:46;%c%%ddd%/%hh%:%mm%:%ss%[/eventtimer][/highlight]
![](https://upload.wikimedia.org/wikipedia/commons/thumb/2/23/Seal_of_the_US_Air_Force.svg/120px-Seal_of_the_US_Air_Force.svg.png)
Viewing the Launch Live:
Live broadcast will be available at 7:26 a.m. PDT / 10:26 a.m. EDT / 14:26 UTC on launch day on the ULA Web site.
The broadcast [eventtimer]2014-04-03 14:26?will start in|started;%c% %h% hours, %m%[/eventtimer] minutes[eventtimer]2014-04-03 14:26?.| ago.;%c%[/eventtimer]
The broadcast [eventtimer]2014-04-03 14:26?will start in|started;%c% %h% hours, %m%[/eventtimer] minutes[eventtimer]2014-04-03 14:26?.| ago.;%c%[/eventtimer]
Mission Description:
DMSP is a space- and ground-based system used to collect and disseminate timely global
environmental data to the Department of Defense and other governmental agencies. This environmental data consists of visible and infrared cloud cover and other specialized meteorological, oceanographic, and solar-geophysical information required to support the war fighter. DMSP satellites “see” environmental features such as clouds, bodies of water, snow, fire, and pollution in the visual and infrared spectra. The data can be used to determine cloud type and height, land and surface water temperatures, water currents, ocean surface features, ice, and snow.
DMSP data are processed on the ground, interpreted by meteorologists, and ultimately used in planning and conducting U.S. military operations worldwide.
Each satellite has an orbital period of about 101 minutes and crosses any point on the Earth up to twice a day, thus providing nearly complete global coverage of clouds every six hours. The visible and infrared sensors collect images of global cloud distribution across a 3,000-km
swath during both daytime and nighttime conditions. The coverage of the microwave imager and sounders are one-half the visible and infrared sensors coverage. They cover the polar regions above 60 degrees twice daily and the equatorial region once daily.
The DMSP is composed of the space segment; the command, control, and communications segment (C3S); and the user segment. The principal function of the space segment is to continually acquire environmental data through its satellite sensors. Mission data downlinks include stored data and real-time transmissions. Raw sensor data are stored onboard the satellite for
delayed transmission to the C3S. Subsequently, the data are relayed to strategic elements of the user segment for ground processing into environmental data records and analysis. Raw data can also be transmitted directly from the space segment to tactical elements of the user segment for
ground processing and analysis.
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Operator:|
Contractors:|
Equipment:|
Configuration:|
Dimensions:|
Launch Weight:|
Orbit:|
Photos:|
environmental data to the Department of Defense and other governmental agencies. This environmental data consists of visible and infrared cloud cover and other specialized meteorological, oceanographic, and solar-geophysical information required to support the war fighter. DMSP satellites “see” environmental features such as clouds, bodies of water, snow, fire, and pollution in the visual and infrared spectra. The data can be used to determine cloud type and height, land and surface water temperatures, water currents, ocean surface features, ice, and snow.
DMSP data are processed on the ground, interpreted by meteorologists, and ultimately used in planning and conducting U.S. military operations worldwide.
Each satellite has an orbital period of about 101 minutes and crosses any point on the Earth up to twice a day, thus providing nearly complete global coverage of clouds every six hours. The visible and infrared sensors collect images of global cloud distribution across a 3,000-km
swath during both daytime and nighttime conditions. The coverage of the microwave imager and sounders are one-half the visible and infrared sensors coverage. They cover the polar regions above 60 degrees twice daily and the equatorial region once daily.
The DMSP is composed of the space segment; the command, control, and communications segment (C3S); and the user segment. The principal function of the space segment is to continually acquire environmental data through its satellite sensors. Mission data downlinks include stored data and real-time transmissions. Raw sensor data are stored onboard the satellite for
delayed transmission to the C3S. Subsequently, the data are relayed to strategic elements of the user segment for ground processing into environmental data records and analysis. Raw data can also be transmitted directly from the space segment to tactical elements of the user segment for
ground processing and analysis.
Specifications
Type / Application:
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- Meteorology
Operator:|
- USAF
Contractors:|
- Lockheed Martin
Equipment:|
- OLS Operational Linescan System
- SSMIS Microwave Imager and Sounder
- SSJ/5 Precipitating Electron and Ion Spectrometer
- SSULI Ultraviolet Limb Imager
- SSUSI Ultraviolet Spectrographic Imager and Nadir Airglow Photometer
- SSI/ES-3 Thermal Plasma Instrument
- SSF Laser Threat Warning Sensor
Configuration:|
- Tiros-N bus
Dimensions:|
- 14 feet tall, 25 feet width with solar panels deployed
Launch Weight:|
- ~1200 kg (~2700 lb) - max wet weight at launch
Orbit:|
- SSO (857 km × 857 km; 99° inc.)
Photos:|
![20091019-dmsp-hr.jpg](http://www.spacemankind.com/images/ms/20091019-dmsp-hr.jpg)
Mission Insignia (clickable)
![fairingfull.jpg](http://www.spaceflightnow.com/atlas/av044/images/fairingfull.jpg)
![dmsppatch.jpg](http://www.spaceflightnow.com/atlas/av044/images/dmsppatch.jpg)
![DMSPF1901.jpg](https://dl.dropboxusercontent.com/u/102519027/DMSPF1901.jpg)
Launch preparations photos:
DMSP 19 mated to Atlas 5 for launch (PHOTO GALLERY)
Launch Updates:
- Spaceflight Now's Mission Status Center
- United Launch Alliance Twitter
- ULA launch hotline - dial at: 1-877-852-4321
Launch Vehicle:
The Atlas 5 was developed by Lockheed Martin Commercial Launch Services as part of the US Air Force Evolved Expendable Launch Vehicle (EELV) program. Each Atlas 5 rocket uses a Russian-built RD-180 engine burning kerosene and liquid oxygen to power its first stage and an American-built RL10 engine burning liquid hydrogen and liquid oxygen to power its Centaur upper stage.
The Atlas 5 launcher will fly in the so-called 401 configuration, denoting a 4-meter payload fairing, no strap-on solid rocket boosters and a single-engine Centaur upper stage.
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The Atlas 5 launcher will fly in the so-called 401 configuration, denoting a 4-meter payload fairing, no strap-on solid rocket boosters and a single-engine Centaur upper stage.
Specifications
Gross mass:
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- 338640 kg (746570 lb)
Payload:
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- 7095 kg (15641 lb) SSO
- 4950 kg (10910 lb) GTO
Height:
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- 58.30 m (191.20 ft)
Diameter:
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- 3.81 m (12.49 ft)
Span:
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- 3.81 m (12.49 ft)
Thrust:
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- 3827.00 kN (860343 lbf)
Launch Timeline & Ground Track:
![DMSPF1902.jpg](https://dl.dropboxusercontent.com/u/102519027/DMSPF1902.jpg)
![DMSPF1903.jpg](https://dl.dropboxusercontent.com/u/102519027/DMSPF1903.jpg)
Weather Forecast for Vandenberg AFB, California on April 3, 2014 (8 a.m.)
Partly to mostly cloudy. High near 16C. Winds W at 15 to 25 kmh.
6 AM|8°C|6°C|87%|0%|0%|6%|1018 hPa|6 km/h E|
![clear.gif](http://icons-ak.wxug.com/i/c/k/clear.gif)
Links: