DMSP

Description

Platform

DMSP

Summary

DMSP (Defense Meteorological Satellites Program) is a series of environmental and weather satellites operated by US Air Force, whose first element was launched in June 2007. Onboard instruments relevant for oceanography include the SSM/I microwave imager, a passive sensor measuring brightness temperature over the sea surface which can be used to determine sea ice concentration or surface wind speeds.

Agency

US Air Force

Orbit

polar orbiting (altitude 800 km)

Launch date

19/06/1987

Status

Operational

Involvement of CERSAT

The radiometric data from the onboard SSM/I sensor are downloaded from NASA/GFDC at CERSAT to study air-sea fluxes, polar sea-ice and ocean winds and they are used in the processing of many of the related products. Only SSM/I data from F10, F11, F13 and F14 satellites of the DMSP series are mirrored at CERSAT.

The DMSP satellites

The first satellite, F8, was launched on June 19, 1987, aboard the Defense Meteorological Satellite Program (DMSP). For the first time, it takes on board a new type of Special Sensor Microwave Imager (SSM/I) and a Special Sensor Microwave Temperature (SSM/T-I).

This satellite orbit is near-circular , sun-synchronous, and near-polar. The F08 orbital altitude is near 833 km, with a 98.8 ° inclination, and 102 mn orbital periods. It executes 14.1 revolutions per day and the local time for the ascending equatorial crossing is 6:12 am. The swath is about 1400 km wide.

The SSM/I instrument

Goals

As it was defined by N.S.S.A. and A.F.S.D., the SSM/I program consists in obtaining a world wide athmospheric parameters which have a high importance for the meteorology and climatology.

  • athmospheric water vapor content
  • athmospheric water liquid content (cloud) and rain rates
  • wind speed on ocean surfaces
  • ground humidity
  • snow surfaces detection and water content analysis
  • sea-ice detection and concentration
  • sea-ice characterisation

Characteristics

The SSM/I was built by Hughes Aircraft Company under the management of N.S.S.A (Naval Space System Activity) and A.F.S.D (Air Force Space Division).

The SSM/I consists of 7 separate total-power radiometers, each simultaneously measuring the microwave emission coming from the Earth and the intervening atmosphere. Table 1 gives the frequencies, polarizations, and temporal and spatial resolution for the 7 channels. Dual-polarization measurements are taken at 19;35, 37.0, and 85.5 GHz, and vertical polarization is observed at the 22.235 GHz [water vapor channel] (Figures 1 & 2).

ssmi_f1
ssmi_f2

Figure 1 : F08 SSM/I orbit and scangeometry (from Hollinger 1989)

Figure 2 : Geometric representation ofSSM/I scan (from Spencer et al., 1989)

A two step scanning :

  • A-scan : during the 102.4 arc of an A-scan, 64 samples of each of the lower channels are taken, with the integration period being 7.95 ms. During each scan, the 85 GHz channels are sampled 128 times over the 102.4° arc. This sampling scheme results in 128 pol footprints, each having an effective 3dB spatial resolution of 15 km.
  • B-scan : Only the 85 GHz channels are realised giving again 128 pol footprints (Figure 1).

There are 1579 A or B-type pairs per orbit.

Channels

1,2

3

4,5

6,7

Central Frequency Pol. (GHz)

19.35

22.24

37.0

85.5

Radiometric Pol. (V/H) (*)

V ,H

V

V ,H

V, H

Thermal resolution (K)

0.8

0.8

0.6

1.1

Integrated FOV (Km)

70 x 45

60 x 40

38 x 30

16 x 14

Spatial sampling (Km)

25

25

25

12.5

Scan angle

   

102.4 °

 

Sweep periodicity

   

1.9s

 

Ground incidence

   

53.1°

 

Swath width

   

1394 Km

 

Antenna diameter

   

65 cm

 

Weight

   

120 Kg

 

Power

   

70 W