The Defense Meteorological Satellite Program (DMSP) provides global visible and infrared cloud data and other specialized meteorological, oceanographic and solar-geophysical data in support of worldwide Department of Defense (DoD) operations. The DMSP F10 satellite, launched in December 1990, is in a near circular, sun synchronous, polar orbit. This document describes the DMSP mission, the satellite, and its environment. The document also briefly describes the ground data system. Separate platform description documents are available for the F8, F11, F13, F15, and F17 satellites.
1. Platform or Data Collection Environment Overview
2. Ground Segment Information
3. References
4. Glossary of Terms
5. Acronyms and Abbreviations
6. Document Information
Defense Meteorological Satellite Program (DMSP) Block 5D-2 Satellite F10, DMSP F10
DMSP, originally known as the Defense System Applications Program (DSAP) and the Defense Acquisition and Processing Program (DAPP), is a long-term USAF effort in space to monitor the meteorological, oceanographic and solar-geophysical environment of the Earth in support of DoD operations. All spacecraft launched have had a tactical (direct readout) and a strategic (stored data) capacity. In December 1972, DMSP data were declassified and made available to the civil and scientific communities. The USAF maintains an operational constellation of two near-polar, sun-synchronous satellites.
Satellite
The DMSP program office is located at the Space Systems Division, Air Force Material Command, Los Angeles Air Force Station, Los Angeles, California 90009-2960. Funding is provided by the Department of Defense (DoD).
The DMSP mission is to provide global visible and infrared cloud data and other specialized meteorological, oceanographic and solar-geophysical data in support of worldwide Department of Defense (DoD) operations.
DMSP Satellite F10 was built by General Electric's Astro-Space Division (now part of Martin Marietta Astro Space) and was launched on December 1, 1990. The spacecraft is 3.7 meters in length with a diameter of 1.2 meters with an on-orbit mass of 831 kilograms. It has a design lifetime of 48 months. Power is provided though a 9.29 sq-m solar cell panel. Attitude is controlled using momentum wheels and magnetic coils using a strap-down star sensor and gyros as the reference.
DMSP Satellite F10 is in a near circular, sun synchronous, polar orbit. The satellite did not achieve the desired orbit, and as a result the orbit is more elliptical than it was designed to be.
pointing accuracy: 0.01 deg (primary), 0.12 deg (backup)
stability: maximum rate = 0.03 deg/sec per axis
Short-term changes in attitude are measured using three orthogonal gyroscopes. A strap down star sensor is used to bound the effects of gyroscope drift. The desired attitude is computed based upon a star catalog and an ephemeris table uplinked to the spacecraft daily. Three-axis attitude control is maintained in the orbital configuration by automatic momentum exchange between three momentum wheels. Onboard magnetic coils provide controlled interaction with the Earth's magnetic field to prevent the accumulation of wheel secular momentum. Operation of these coils is under control of the closed loop spacecraft attitude control system. Both the momentum wheels and gyroscopes are backed up by a fourth skewed unit for redundancy.
Data are transmitted in real time to tactical terminals worldwide. Data are also stored using onboard recorders for transmission to and processing by the Air Force Global Weather Central (AFGWC), Offutt AFB, Nebraska and the Fleet Numerical Meteorology and Oceanography Center (FNMOC), Monterey, California. Both AFGWC and FNMOC relay the SSM/I, SSM/T and SSM/T2 data to the National Environmental Satellite, Data, and Information System (NESDIS). AFGWC also sends the entire data stream to the National Geophysical Data Center (NGDC).
DMSP uses S-band links at 1.024 Mbps for the tactical real time transmissions. Stored data are transmitted at 2.66 Mbps to receiving sites at:
Data are then relayed at 3.072 Mbps via commercial geostationary communications satellite to AFGWC and FNMOC. Spacecraft commanding is done at L-band at a 2 Kbps rate.
DMSP satellite command and control is performed by the 6th Satellite Operations Group at Offutt AFB, Nebraska.
Data are transmitted in real time to tactical terminals worldwide. Data are also stored using onboard recorders for transmission to and processing by the Air Force Global Weather Central (AFGWC), Offutt AFB, Nebraska and the Fleet Numerical Meteorology and Oceanography Center (FNMOC), Monterey, California. Both AFGWC and FNMOC relay the SSM/I, SSM/T and SSM/T2 data to the National Environmental Satellite, Data, and Information System (NESDIS). AFGWC also sends the entire data stream to the National Geophysical Data Center (NGDC).
ascending equatorial crossing time (local time):
NOTE: The satellite did not achieve the desired orbit, and as a result the equator crossing time is increasing by approximately 45 minutes per year.
Dubach L., and C. Ng. 1988. NSSDC's Compendium of Meteorological Space Programs, Satellites, and Experiments, March 1988.
Kramer, H. J. 1994. Observation of the Earth and its Environment - Survey of Missions and Sensors, 2nd Edition, Springer-Verlag, ISBN: 3-540-578587, May 1994.
OLS: The Operational Linescan System (OLS) measures visible (0.4-1.1 micrometers) and infrared (10.25-12.6 micrometers) wavelengths to provide day and night cloud cover imagery. The satellite measures data at a 0.56 km resolution, which is averaged on board, to produce global coverage at 2.7 km resolution. All of the 2.7 km resolution (smooth) data are downlinked to the ground sites while a small amount of the 0.56 km resolution (fine) data are stored and downlinked. The OLS is the primary sensor on each DMSP satellite.
SSM/I: Special Sensor Microwave Imager.
SSM/T-1: Special Sensor Microwave Temperature Sounder. The SSM/T is a seven channel, cross track nadir scanning passive microwave sounder having a field of view of 14.4 degrees. It measures the Earth surface and atmospheric emission in the 50 to 60 GHz oxygen band. At nominal altitude, the subtrack spatial resolution is an circle of 174 km at nadir and an ellipse of 213x304 km toward the limb. There are seven total cross-track scan positions separated by 12 degrees at frequencies 50.5, 53.2, 54.35, 54.9, 58.4, 58.825 and 59.4 GHz.
SSJ/4: Precipitating Plasma Monitor. The SSJ/4 measures the transfer energy, mass, and momentum through the magnetosphere-ionosphere in the Earth's magnetic field. The SSJ/4 sensor consists of four electrostatic analyzers that record the flux of precipitating ions or electrons at 20 fixed energy channels between 50 eV and 30 keV.
SSIES: Special Sensor Ionspheric Plasma Drift/Scintillation Meter. The SSIES measures the ambient electron density and temperatures, ambient ion density, the average ion temperature and molecular weight, the plasma drift and scintillation at the DMSP orbital altitude.
SSBX-2: Gamma Ray Particle Detector. The SSB/X-2 is an array-based system that detects the location, intensity, and spectrum of X-rays emitted from the Earth's atmosphere.
The following acronyms and abbreviations are used in this document.
| AFB | Air Force Base |
| AFGWC | Air Force Global Weather Central |
| DMSP | Defense Meteorological Satellite Program |
| DoD | Department of Defense |
| eV | Electron Volts |
| FNMOC | United States Navy Fleet Numerical Meteorology and Oceanography Center |
| GHz | Gigahertz |
| kbps | Kilobits Per Second |
| keV | Kilo Electron Volts |
| Mbps | Megabits Per Second |
| NESDIS | National Environmental Satellite, Data, and Information Service |
| NGDC | National Geophysical Data Center |
| OLS | Operational Linescan System |
| SSBX-2 | Special Sensor Gamma Ray Particle Detector |
| SSIES | Special Sensor Ionospheric Plasma Drift/Scintillation Meter |
| SSJ/4 | Special Sensor Precipitating Plasma Monitor |
| SSM/I | Special Sensor Microwave Imager |
| SSM/T-1 | Special Sensor Microwave Temperature Sounder |
| USAF | United States Air Force |
| URL | Uniform Resource Locator |
Revision Date: MSFC: September 19, 1995; NSIDC: September 25, 1996
Review Date: MSFC: September 19, 1995; NSIDC: September 25, 1996
Document ID: DMSP F-10 Platform Document
Document Curators: NSIDC Writers
Document URL: http://nsidc.org/data/docs/daac/f10_platform.gd.html