08 VEEBR. 2002 Avaldamiskuupäev 6896 Vaatamised

Multi-spectral data from 20 channels are obtained from a single scanning telescope. A rotating filter wheel located in the optical train containing 20 individual filters seperates the individual channels. An elliptical scan mirror provides cross-track scanning of 56 steps in increments of 1.8°. The filter wheel makes one revolution for each step of the scan mirror. The mirror rapidly steps (@ 32 msec.), then holds at each position while the 20 filter segments are sampled during the wheel revolution. This action ('stop & stare') takes place each 0.1 sec. As a result, an Earth scan line lasts 6.4 sec. (stops & stares + retrace back).

The HIRS/4 optics are designed to operate within its specifications under any Sun angle condition between 0° and 80°. The radiant cooler is designed to operate from 0° to 68° Sun angle and, with spacecraft supplied shading, can operate from 0° to 80° Sun angle. The Sun angle is defined as the angle between the satellite to Sun line and the normal to the orbital plane.

HIRS/4 scans the Earth surface in 20 spectral bands in the range of 0.69 - 14.95 microns: one visible channel at 0.69 micron, seven short-wave IR channels (3.7 to 4.6 microns) and 12 long-wave IR channels (6.5 to 15 microns). This provides data for:

  • temperature

  • altitude profiles

  • moisture content

  • cloud height

  • surface albedo

The instrument sensitivity (noise equivalent spectral radiance, NEDN) are illustrated in the table below.

Channel number

Centre wavenumbCener (cm-1)

tre wavelength (mm)

Specified sensitivity (NEΔN) (mW/
m2 sr
cm-1)

FWHM bandwidth (cm-1)

1

669

14.95

3.00

3

LW 

2

680

14.71

0.67

10

LW

3

690

14.49

0.50

12

LW

4

703

14.22

0.31

16

LW

5

716

13.97

0.21

16

LW

6

733

13.64

0.24

16

LW

7

749

13.35

0.20

16

LW

8

900

11.11

0.10

35

LW

9

1030

9.71

0.15

25

LW

10

802

12.47

0.15

16

LW

11

1365

7.33

0.20

40

LW

12

1533

6.52

0.20

55

LW


13         

2188             

4.57          

0.006   

23            

SW

14

2210

4.52

0.003

23

SW

15

2235

4.47

0.004

23

SW

16

2245

4.45

0.004

23

SW

17

2420

4.13

0.002

28

SW

18

2515

4.00

0.002

35

SW

19

2660

3.76

0.001

100

SW

20

14500

0.69

0.10% albedo

1000

VIS

The HIRS/4 instrument is a single package that mounts directly onto the satellite. The major sub-assemblies are:
  • Scan subsystem

  • Filter Wheel Sub-Assembly

  • Detectors

  • Radiant Cooler Assembly

  • Optical Assembly

  • Baseplate


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