The Millime ter Regime Crystal Brogan (NRAO/NAASC) MOPRA Austral ia 22m LMT Mexico 50m APEX Chil e 12m IRAM 30m Spain Nobeyama Japan 45m CSO Hawaii 10.4m JCMT Hawaii 15m SMT Arizon a 10m Onsala Sweden 20m GBT West Virginia 100m ASTE Chil e 10m ARO 12m Arizona
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The Millimeter Regime Crystal Brogan (NRAO/NAASC) MOPRA Australia 22m LMT Mexico 50m APEX Chile 12m IRAM 30m Spain Nobeyama Japan 45m CSO Hawaii 10.4m.
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The Millimeter RegimeCrystal Brogan
(NRAO/NAASC)
MOPRA Australia
22m
LMT Mexico
50m
APEX Chile 12m
IRAM 30m Spain
Nobeyama Japan
45m
CSO Hawaii 10.4m
JCMT Hawaii
15m
SMT Arizona
10m
Onsala Sweden
20m
GBT West Virginia
100m
ASTE Chile 10m
ARO 12m Arizona
The Millimeter RegimeCrystal Brogan
(NRAO/NAASC)
MOPRA Australia
22m
LMT Mexico
50m
APEX Chile 12m
IRAM 30m Spain
Nobeyama Japan
45m
CSO Hawaii 10.4m
JCMT Hawaii
15m
SMT Arizona
10m
Onsala Sweden
20m
GBT West Virginia
100m
ASTE Chile 10m
ARO 12m Arizona
Outline
• Effect of the Atmosphere at mm wavelengths
• Effective System Temperature
• Direct Method of mm calibration
• Simplified formulation of Chopper Wheel method of mm calibration
• More accurate approach
• Efficiencies and different ways of reporting temperature
• Why is mm so interesting?
Problems unique to the mm/sub-mm
• Atmospheric opacity is significant for λ<1cm: raises Tsys and attenuates source
– Varies with frequency and altitude
– Changes as a function of time mostly due to H2O
– Causes refraction which leads to pointing errors – Gain calibration must correct for these atmospheric effects
•Hardware
–Noise diodes such as those used to calibrate the temperature scale at cm wavelengths are not available at mm to submm wavelengths
•Antennas–Pointing accuracy measured as a fraction of the beam (PB ~ 1.22 /D) is more difficult to achieve–Need more stringent requirements than at cm wavelengths for: surface accuracy and optical alignment
Constituents of Atmospheric Opacity
• Due to the troposphere (lowest layer of atmosphere): h < 10 km
• Temperature decreases with altitude: clouds & convection can be significant
• Dry Constituents of the troposphere:, O2, O3, CO2, Ne, He, Ar, Kr, CH4, N2, H2
• H2O: abundance is highly variable but is < 1% in mass, mostly in the form of water vapor
• “Hydrosols” (i.e. water droplets in the form of clouds and fog) also add a considerable contribution when present
Troposphere
Stratosphere
Column Density as a Function of Altitude
Opacity as a Function of PWV (PWV=Precipitable Water Vapor)
Optical Depth as a Function of Frequency
• At 1.3cm most opacity comes from H2O vapor
• At 7mm biggest contribution from dry constituents
• At 3mm both components are significant
• “hydrosols” i.e. water droplets (not shown) can also add significantly to the opacity
43 GHz
7mm
Q band
22 GHz
1.3cm
K band
total optical depth
optical depth due to H2O vapor
optical depth due to dry air
100 GHz
3mm
MUSTANG
Effect of Atmosphere on Pointing
• Since the refractive index of the atmosphere >1, an electromagnetic wave propagating through it will be bent which translates into a pointing offset
The index of refraction
-Pointing off-sets Δθ ≈ 2.5x10-4 x tan(i) (radians)
@ elevation 45o typical offset~1’
- GBT beam at 7mm is only 15”!
atm
waterdry
T
PPn
1
The amount of refraction is strongly dependent on the elevation
In addition to receiver noise, at millimeter wavelengths the atmosphere has a significant brightness temperature:
Tsys ≈ Trx + Tsky
where Tsky =Tatm (1 – e)
so Tsys ≈ Trx +Tatm(1-e)
Sensitivity: System noise temperature
Receiver temperature
Emission from atmosphere
Before entering atmosphere the signal S= Tsource
After attenuation by atmosphere the signal becomes S=Tsource e-
(Tatm = temperature of the atmosphere ~ 270 K)
Consider the signal to noise ratio:
S / N = (Tsource e-) / Tsys = Tsource / (Tsys e)
Tsys* = Tsys e ≈ Tatm(e + Trxe
The system sensitivity (S/N) drops rapidly (exponentially) as opacity increases
Effective System Temperature
*
Atmospheric opacity, continued
Typical optical depth for 230 GHz observing at the CSO:
at zenith225 = 0.15 = 3 mm PWV, at elevation = 30o 225 = 0.3
Tsys*(DSB) = e(Tatm(1-e-) + Trec)1.35(77 + 75) ~ 200 K
assuming Tatm = 300 K
Atmosphere adds considerably to Tsys and since the opacity can change rapidly, Tsys must be measured often
Many MM/Submm receivers are double sideband, thus the effective Tsys for spectral lines (which are inherently single sideband) is doubled
Tsys*(SSB) = 2 Tsys (DSB) ~ 400 K
Direct Method of MM CalibrationTA’ is the antenna temperature of the source corrected as if it lay outside the atmosphere
rxsky
A
rxsky
rxskyrxskyA
TT
eT
TT
TTTTeT
'
)()'(
off
offon
V
VV
l
AA
TT
'
* Where ηl accounts for ohmic losses, rear spillover, and scattering and is < 1
' eTV
VVT sys
off
offonA
Inverting this equation at the observing frequency must be obtained by a tipping scan or some other means
This is the method used at the GBT
Direct Calibration of the Atmosphere eTTeTTTT CBRlspilllatmlRx
skyAsys )1()1(
Ael oo eee )sin(/
With enough measurements at different elevation, ηl and can be derived as long as reasonable numbers for the other parameters are known
Trx: Receiver temp. from observatory
Tatm ~ 260 K
Tspill: Rear spillover temperature ~300 K
Tcmb = 2.7 K
ηl accounts for ohmic losses, rear spillover, and scattering and is < 1
Tipping scan
eTT syssys *
Down side of the Direct Method
http://www.gb.nrao.edu/~rmaddale/Weather/index.htmlFor a forecast of current conditions
•Atmosphere changes too rapidly to use average values
•Tipping scans use considerable observing time ~10min each time
Probably not done often enough Assume a homogeneous, plane-parallel atmosphere though the sky is lumpyDone as a post-processing step so if something went wrong you’re out of luck
Ael oo eee )sin(/
1
Y
YTTT COLDHOT
RX
][][]/[
COLDRXHOTRX
COLDHOT
VVVV
TTVoltKelvinsg
Determining the Trx and the Temperature Scale
COLDRX
HOTRX
VV
VVY
Then
and
V
TTcold Thot
Vcold +V rx
Vhot + V rx
Treceiver
In order to measure Trx, you need to make measurements of two calibrated ‘loads’:
Tcold = 77 K liquid nitrogen load
Thot = room temperature load
and the temperature conversion factor is
• Trx is not a constant, especially for mm/submm receivers which are more difficult to tune to ideal performance.
• A significant improvement to the Tsys* measurement can be made if Trx is measured rather than assumed
• Currently the SMA and soon ALMA will use a two temperature load system for all calibration
Chopper Measurement of Tsys*
• So how do we measure Tsys* without constantly measuring Trx and the
opacity? Tsys* ≈ TrxeTatm(e
• At shorter mm λ, Tsys* is usually obtained by occasionally placing an
ambient temperature load (Thot) that has properties similar to a black body in front of the receiver.
• We want to know the effective sensitivity, not how much is due to the receiver vs. how much is due to the sky. Therefore, we can use:
offload
off
hotsys VV
VTT
*
Voff is the signal from the sky (but not on source)
Vload is the signal from the hot load
IRAM 30m chopper Blue stuff is called eccosorb
• As long as Tatm is similar to Thot, this method automatically compensates for rapid changes in mean atmospheric absorption
offloadcalcal TTVgT
])1()1([][ spilllatmlRxhotRx TeTTTT
Simplified Load Calibration Theory
Note that the load totally blocks the sky emission, which changes the calibration equations from cm result
Simplify by assuming that
ambatmspillhot TTTT i.e., all our loads are at ambient temp.
eTT amblcalThen most everything cancels out and we are left with
Let
ambhotcal TTT cal
caloffonoffon T
TTTT
)(
Recall from cm signal processing
But instead of diode we have a BB load so
*1
)( Al
A
loffonoffon T
e
T
eTTT
and
offload
hotoffonA TT
TTTT
)(*
So How Does This Help?
Relating things back to measured quantities:
So all you have to do is alternate between Ton and Toff and occasionally throw in a reading of Thot (i.e. a thermometer near your hot load) and a brief observation with Tload in the beam
The poorer the weather, the more often you should observe Tload . This typically only takes a few seconds compared to ~10min for a tipping scan
*1
)( Al
A
loffonoffon T
e
T
eTTT
To first order, ambient absorber (chopper wheel) calibration corrects for atmospheric attenuation!
Millimeter-wave Calibration Formalism
1)/exp(
/),(
kTh
khTJ
Corrections we must make:
1. At millimeter wavelengths, we are no longer in the R-J part of the Planck curve, so define a Rayleigh-Jeans equivalent radiation temperature of a Planck blackbody at temperature T.
ambchopspillatm TTTT
2. Let all temperatures be different:
Linear part is in R-J limit
Once the function starts to curve, the assumption breaks down
3. Most millimeter wave receivers using SIS mixers have some response to the image sideband, even if they are nominally “single sideband”. (By comparison, HEMT amplifiers probably have negligible response to the image sideband.)• The atmosphere often has different opacity in the signal &
image sidebands• Receiver gain must be known in the signal sideband
1 si GG
Gs = signal sideband gain, Gi image sideband gain.
)exp(
)(1*
skyRxs
i
sys
TTG
G
T
fss
AR
TT
*
*
Commonly used TR* scale definition (recommended by Kutner and Ulich):
• TR* includes all telescope losses except direct source coupling of the forward beam in d
• The disadvantage is that fss is not a natural part of chopper wheel calibration and must be included as an extra factor
• TA* is quoted most often. Either convention is OK, but know which one the observatory is using
*
*
Mfss
AMB
TT
If the source angular extent is comparable to or smaller than the main beam, we can define a Main Beam Brightness Temperature as:
Main Beam Brightness Temperature
M* -- corrected main beam efficiency – can measure from observations of planets which have mm Tb ~ few hundred K
][)(
][**
PlanetTdisk
PlanetT
Bcfss
AM
2
2lnexp1)(beam
diskc disk
fss the forward spillover and scattering can be measured from observations of the Moon, if moon = diffraction region
)(
)(*
moonT
moonT
B
Afss
pA
Av A
kTS
2
pA
Alv A
kTS
2*
Conventional
TA* definition
Flux conversion factors (Jy/K)
• mm/submm photons are the most abundant photons in the spectrum of most spiral galaxies – 40% of the Milky Way Galaxy
• After the 3K cosmic background radiation, mm/submm photons carry most of the radiative energy in the Universe
• Probe of cool gas and dust
Why do we care about mm/submm?
Science at mm/submm wavelengths: dust emission
In the Rayleigh-Jeans regime, h« kT,
S= 2kT2 Wm-2 Hz-1
c2
and dust opacity,
so for optically-thin emission, flux density
S
emission is brighter at higher frequencies
Galactic star forming region NGC1333
Spitzer/IRAC image from c2d with yellow SCUBA 850 µm contours
•Dust mass
•Temperature
•Star formation efficiency
•Fragmentation
•Clustering
Jørgensen et al. 2006 and Kirk et al. 2006
Unique mm/submm access to highest z
Andrew Blain
SED of Arp 220 at z=0.02Redshifting the steep FIR dust SED peak counteracts inverse square law dimming
Increasing z redshifts peak
SED peaks at ~100 GHz for
z~10!
Science at mm/sub-mm wavelengths: molecular line emission
• Most of the dense ISM is H2, but H2 has no permanent dipole moment use trace molecules
Plus: many more complex molecules (e.g. N2H+, CH3OH, CH3CN, etc)
The GBT PRIMOS Project:Searching for our Molecular Origins
Hollis, Remijan, Jewell, Lovas
Many of these lines are currently unidentified!
Detection of Acetamide (CH3CONH
2):
The Largest Molecule with a Peptide Bond(Hollis et al. 2006, ApJ, 643, L25)
Detected in emission and absorption toward Sagittarius B2(N) using four A-species and four E-species rotational transitions. All transitions have energy levels less than 10 K.
This molecule is interesting because it is one of only two known interstellar molecules containing a peptide bond.
Thus it could provide a link to the polymerization of amino acids, an essential ingredient for life.
GBT at 7mm
Telescope altitude diam. No. A range (feet) (m) dishes (m2) (GHz)