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A shell 100 AU in diameter at 60K enclosing the 3.84e26 Watt sun. Peak emissions at 48μm and a power flux of 0.1366 W/m^2^. The in-band fraction of total black body emissions as a function of the mean wavelength λ and the wavelength concentration λ/Δλ can be computed from this C program: [[ attachment:irin01.c ]]. The program expects three command line arguments - temperature T , λ, and λ/Δλ. '''irin01''' computes various parameters, including the fraction of total power in-band. It is a bit of a kludge! A shell 100 AU in diameter at 60K enclosing the 3.84e26 Watt sun. Peak emissions at 48μm and a power flux of 0.1366 W/m^2^. The in-band fraction of total black body emissions as a function of the mean wavelength λ and the wavelength concentration λ/Δλ can be computed from this C program: [[ attachment:irin01.c ]]. The program expects three command line arguments - temperature T , λ, and λ/Δλ, then computes various parameters, including the fraction of total power in-band. It is a bit of a kludge!

Infrared Telescopes


Jansky Units and Infrared Radio Telescopes

1 Jansky is 1e-26 W/m2-Hz. Hz implies bandwidth. The bandwidth of a radio telescope is obvious - the bandwidth in Hertz, probably after a chilled reflector into a chilled low noise amplifier, then through a filter. A wider filter picks up more power, and more thermal noise. So the power in Janksy units for a source is Jy = 1e26 * Power~Received / ( Area * ( f_2 - f_1 ) with power in watts, Area of the receiving surface in square meters, and frequencies in Hertz.

Infrared telescopes have much wider bandwidth, and infrared is typically characterized with wavelength (usually micrometers) rather than Hertz. We can recast the formula as

Jy~=~1e26*(P/A)*c*(1/\lambda_2-1/\lambda_1)~=~1e26*(P/A)*c(\lambda_1-\lambda_2)/(\lambda_1\lambda_2)

where c is the speed of light. Defining \Delta\lambda~=~\lambda_1-\lambda_2 and center wavelength \lambda = \sqrt{\lambda_1\lambda_2}, this simplifies to:

Jy ~=~ 1e26*(P/A)*c~\Delta\lambda/\lambda^2

So, how much is that? A parsec is 3.26 light years or 3.0857e16 meters, like a star that appears to move one arcsecond in the sky as the earth moves 1 AU across its orbit. So, a sphere 1 AU in diameter would appear one arc-second across from 1 parsec away. From 200 parsecs away ( 6.1714e18 meters ), a sphere 100 AU in radius or 200 AU in diameter, and heated by the entire sun's output (3.86e26 W), would be about 60K, and deposit all that power on a 200 parsec diameter sphere with an area of 4.786e38 square meters, a power density of 8.07e-13W/m2. We still don't know enough to compute the Jansky units, because we don't know the bandwidth. That is a function of the filtering and imager on our telescope - and if the telescope is not in orbit, the passband and emissions of the atmosphere.

Dyson Server Sky

A shell 100 AU in diameter at 60K enclosing the 3.84e26 Watt sun. Peak emissions at 48μm and a power flux of 0.1366 W/m2. The in-band fraction of total black body emissions as a function of the mean wavelength λ and the wavelength concentration λ/Δλ can be computed from this C program: irin01.c. The program expects three command line arguments - temperature T , λ, and λ/Δλ, then computes various parameters, including the fraction of total power in-band. It is a bit of a kludge!

James Webb Space Telescope

NASA's JWST Mid Infrared Instrument (MIRI), scheduled to deploy in 2018, will be the most powerful long distance infrared imager available, with a 6.5 meter mirror. The imager is a 1024x1024 pixel Raytheon Si:As sensor chip assembly (SCA) with 25 µm pixels. The pixels are 0.11 arcseconds. JWST seems to be optimized for looking for liquid water.

  • This table gives the sensitivity, recomputed below,

    • (detection limit, 10 sigma, 10,000 seconds)
  • Assuming 3.84e26 Watts, The point source detection distance is sqrt( fraction * 3.84e26 / 4 π 3.0857e16 2 sensitivity ) parsecs

    • = 1.8e-4 sqrt( fraction / sensitivity ) parsecs.

λ

λ/Δλ

sensitivity

λ0

λ1

Δλ

300K power

300K

60K power

60K

μm

μJy

W/m2

μm

μm

μm

fraction

parsec

fraction

parsec

F560W

5.6

5

0.16

1.7e-20

6.19

5.07

1.12

3.22e-02

250000

1.43e-13

0.5

F770W

7.7

3.5

0.25

2.8e-20

8.88

6.68

2.20

1.30e-01

390000

6.32e-09

85

F1000W

10

5

0.54

3.2e-20

11.05

9.05

2.00

1.35e-01

370000

6.72e-07

820

F1130W

11.3

16

1.35

2.2e-20

11.66

10.95

0.71

4.54e-02

370000

1.24e-06

1300

F1280W

12.8

5

0.84

3.9e-20

14.14

11.58

2.56

1.46e-01

350000

3.74e-05

5500

F1500W

15

5

1.39

5.6e-20

16.57

13.57

3.00

1.36e-01

280000

2.79e-04

13000

F1800W

18

6

3.46

9.6e-20

19.56

16.56

3.00

9.66e-02

180000

1.44e-03

22000

F2100W

21

4

7.09

2.5e-19

23.79

18.54

5.25

1.19e-01

120000

7.98e-03

32000

F2550W

25.5

6

26.2

5.1e-19

27.71

23.46

4.25

5.78e-02

19000

1.69e-02

33000

Herschel

ESA's Herschel Space Telescope, active from 2009 to 2013, has a 3.5 meter mirror and a wavelength range of 55 to 672 μm. The Photodetector Array Camera and Spectrometer (PACS) uses two low resolution arrays of bolometers:

Red

16x32

6.4as

Blue

32x64

3.2as

These measure in 3 bands, either 70 alone or 100 and 160 together:

70

60 to 85 μm

5 mJy (5σ, 1h)

100

85 to 130 μm

5 mJy (5σ, 1h)

160

130 to 210 μm

10 mJy (5σ, 1h)

MoreLater

IRtelescope (last edited 2015-07-26 18:40:30 by KeithLofstrom)