Adding Interferometry for CMBPol Peter Timbie University of Wisconsin - Madison

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Adding Interferometry
for CMBPol
Peter Timbie
University of Wisconsin - Madison
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27 August 2008
CMBPol Technology Workshop
1
Imaging and Interferometry
tor
a
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co
Visibilites V(u,v)
FT
Cl
Cl
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CMBPol Technology Workshop
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Outline
Why interferometry?
Challenges
Beam combination: pairwise vs ‘all-on-one’, multiplying vs adding
Guided-wave beam combiner
Quasi-optical beam combiner
MBI
EPIC Interferometer
Required technologies (bolometric interferometer)
horn antenna arrays
OMTs
phase modulators
Discussion
beam combiner/correlator
filters
bolometers/readout
100 mK cooler
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CMBPol Technology Workshop
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CMB
Interferometers
Interferometers
for the CMB
27 August 2008
ν (GHz)
FOV
# ant’s
receivers
DASI
30
5o
13
HEMT
CBI
30
44’
13
HEMT
MINT
150
30’
4
SIS
VSA
30
7o
14
HEMT
BIMA
30
6’
6
HEMT
OVRO
30
4’
9
HEMT
T-W
45
5o
2
SIS
BAM
90-270
42’
2
Bolo
VLA
5, 8, 16
7’
27
HEMT
SZA
30, 90
10’, 3’
8
HEMT
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Why CMB Interferometry? Systematics!
• simple optics
- forms beams with corrugated horn arrays
- symmetric beam patterns, low sidelobes, no mirrors
• no off-axis aberrations
• Stokes U measured by correlation of Ex and Ey on a single detector
(no differencing of detectors)
• differences sky signals without scanning
• measures power spectrum directly
• measures both Temp and Polarization anisotropy
• coherent (HEMTs) or incoherent (bolometers) systems possible
• angular resolution ~ 2X better than imager of equivalent diameter
• CMB polarization first detected with interferometer (DASI)
• simple scan strategy - rotate about optical axis, move on to new pixel
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Interferometer beam systematics:
example
n1
n2
VijU =
∫ dn1 dn2Gix (n1 )G jy (n2 ) Eix (n1 )E jy (n2 )
y
i
x
uij
X
j
U(n1 )e
=
∫
2πiu ij ⋅n 1
dnGix (n)G jy (n)U(n)e
δ(n1 − n2 )
i 2πu ij ⋅n
So - beam mismatch, distortion, etc. do not couple T into
Stokes U visibility measurement.
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Challenges for Interferometry
• beam combiner - scalable, low loss
• “fringe smearing” from wide bandwidths
• simulations
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Beam Combination
1.
2.
Pairwise (Michelson): signals are split and combined pairwise
•
N(N-1)/2 pairs (78 for N = 13, 4950 for N =100)
•
multiplying correlator (coherent receivers only)
a. analog (DASI/CBI)
b. digital (most radio interferometers)
see Coherent Detectors, C. Lawrence et al.
- power?
- bandwidth?
•
adding correlator with bolometers: M. Hattori, Tohoku University
Fizeau (Butler): signals from all antennas appear at all detectors
•
Fizeau approach has lower noise in background-limited case, in low n limit
(Zmuidzinas 2003)
•
Hamilton et al. (astro-ph/0807.0438) compares to imaging
•
Guided-wave adding interferometer (Butler combiner, Rotman lens)
•
Quasioptical adding interferometer using a telescope (MBI)
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Ryle’s Adding Interferometer (1952)
“visibility”
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Adding interferometer for N > 2
E ⊥1 + E||1
E ⊥ 2 + E||2
E ⊥N + E||N
N horns
OMTs
2N phase
modulators
// ⊥ // ⊥
// ⊥
….
beam combiner
detectors
….
( E ⊥1 + E||1 + ...E ⊥N + E|| N )
N
×
( E ⊥1 + E||1 + ...E ⊥N + E|| N ) ∗
N
2
2
(E ⊥1
+ ...E⊥N
) + (E ⊥1 E ||1 + ...E ⊥N E||N ) + (E⊥1 E||2 + ...E⊥1 E||N ) + (E⊥1 E ⊥ 2 + ...E|| E||N )
=
N
total power
single-horn
auto-correlation
Stokes U
visibilities
Stokes I
visibilities 10
I. Guided-wave beam combiner
• Waveguides or planar transmission line
• Butler combiners (N inputs and N outputs)
• Rotman lens (N inputs, > N outputs)
• Losses may restrict to coherent receivers (with gain)
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Rotman Lens interferometer scheme
(see poster by R.A. Watson & L. Piccirillo)
2D horn array (HEMTs)
Rotman Lens stack
Anti-reflection
resistive layer
φφ
φφ
Orthogonal cross stack
φφ
φφ
Geometric
delays
OMTs
T
Q
array
Detector array
Diode
Diode
detector
φφ
Phase
switches
U
Idealised Rotman interferometer scheme showing the input TQU maps and the paths through to the detectors. The signal
from each sky element reaches each horn with different geometric delays. OMTs split the signals into different hands of
polarization which are then phase switched independently before being input to the first Rotman stack. The column followed
by the row stack performs a Fourier transform and the Fourier transform of these detected outputs gives the visibility
information.
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The Rotman Lens: Alternative to Butler combiner
(Watson & Piccirillo)
Antenna ports
A
C
D
Du
mm
yp
ort
s
rt s
po
Rotman lens (Rotman and Turner 1963) is a
planar transmission line implementation of the
quasi-optical combiner.
D
um
m
y
po
rts
rts
po
y
mm
Du
D
my
um
B
-7π /8
-7π /16
7π /16 -5π /8
7π /8 -5π /16 -3π /8
5π /16 -3π /16 -π/8
5π/8 3π /16 -π/16
3π/8 π/16
π/8
7π /8
7π /16
5π/8 -7π /16
3π/8 5π /16 -7π /8
π/8 3π /16 -5π /16
π/16 -3π /16 -5π /8
-π/16 -3π /8
-π/8
Beam ports
HFSS simulation of a Rotman Lens. The relative
phase on the outputs is given in different colours for
each antenna port.
27 August 2008
It consists of a set of beam and antenna ports
either side of a specially shaped parallel plate
cavity through which the waves propagate.
The design is simple and many inputs and outputs
can be easily incorporated, unlike a Butler
combiner
It can be implemented cheaply in microstrip and
using high dielectric constant substrate (εr>10)
can reduce size sqrt(εr) (>3).
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II.
Adding interferometer with a quasioptical beam combiner
• Millimeter-wave Bolometric Interferometer (MBI)
• EPIC Interferometer
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Quasioptical Beam Combiner
Cryostat
Feed horn antennas
Phase Shifters
45° CW twist
rectangular
wave guide
45º CCW twist
rectangular
wave guide
Bolometer Array
Parabolic mirror
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The Millimeter-Wave Bolometric
Interferometer (MBI)
Antennas
• Fizeau (optical) beam combiner
Phase modulators
• 4 feedhorns (6 baselines)
• 90 GHz (3 mm)
• ~1o angular resolution
• 7o FOV
Liquid nitrogen tank
Liquid helium tank
Secondary mirror
3
He refrigerator
Primary mirror
Bolometer unit
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Effect of Phase Shifting
Single Baseline
Six baselines
(Two feeds)
(Four feeds)
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MBI Assembly
15 cm
19 spider-web bolos (JPL)
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MBI Team
Brown University
Greg Tucker, Andrei Korotkov
Jaiseung Kim
University of Richmond
Ted Bunn
University of Manchester
Lucio Piccirillo
Cardiff University
Peter Ade, Carolina Calderon
National University of Ireland - Maynooth
Creidhe O’Sullivan, Gareth Curran
University of Wisconsin - Madison
Peter Timbie, Amanda Gault
Peter Hyland, Siddharth Malu
University of Illinois
Ben Wandelt
UC San Diego
Evan Bierman, Brian Keating
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First light
at
Pine Bluff Observatory
Madison, WI
March 2008
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MBI interference fringes
Tucker et al. SPIE 2008
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Einstein Polarization Interferometer for
Cosmology (EPIC) Mission Concept
25 cm at
λ = 0.3 cm
Corrugated horns
OMTs
RF phase modulators
Fizeau beam combiner
Backshort Under Grid (BUG)
TES array (NASA/GSFC)
64-element module
(1 of 16)
Interference fringes measured in
focal plane by bolometer array
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EPIC LEO Mission Concept
250 GHz
90 GHz module
(1 of 8) 0.25 m dia
150 GHz
60 GHz
30 GHz
0.9 m
1.75 m dia
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EPIC LEO Mission Concept
• Measure CMB E and B mode polarization over full sky to
foreground limit (T/S ~ 0.01)
ƒ Scaled close-packed corrugated horn arrays: 30-300 GHz
ƒ ~15o FOV, ~ 1o synthesized beams
ƒ Total # horns N ~ 1024 (= # modes) x 2 pol’ns
ƒ Interferometer: signals cross-correlated
- between horns: N(N-1)/2 visibilities for small scales Arrays
- between 2 polarizations for each horn:
“correlation polarimetry” for large scales
LHe Dewar
ƒ Lifetime > 1yr from 900 km Earth orbit (COBE)
Spacecraft Bus
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EPIC sensitivity calculation
•
•
•
•
•
•
•
•
•
•
•
each array module has N = 64 antennas, 2 polarizations
signal from each antenna spread out over focal plane of
4N = 256 detectors
phase-modulated fringe signal meas’d independently
by each detector
background-limited detectors in focal plane of beam combiner
η = 0.5, 20 % BW
4N demodulated signals are then added in quadrature
to compute visibility
repeat for each of the 2N(2N-2)/2 visibilities (all baselines)
add in quadrature signals from other arrays at 90 GHz
1 - year integration over full sky (“Knox” formula)
see J. C. Hamilton et al. (astro-ph/0807.0438)
- comparison with imager, coherent interferometer
- simulation
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EPIC Sensitivity
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Interferometer “Fringe Smearing”
• 1-D simulation
• diffuse source
(CMB) with flat
power spectrum
• horn aperture
D ~ 17λ
~7° FWHM beam
QuickTime™ and a
decompressor
are needed to see this picture.
horn
spacing
D
2D
4D
6D
8D
12D
16D
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Horn Antenna Arrays
• need close-packed arrays of ~ 8 x 8 antennas
from 30 GHz to 300 GHz
• total of 1024 horns for EPIC Interferometer
• platelet arrays (see Gundersen and Wollack)
• smooth-walled horns (Yassin et al.)
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G. Yassin
Easy machining!
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30
Ortho-mode transducers
• separate X/Y linear or R/L circular polarization modes
• input: interface to circular horn output
• output: interface to phase modulator (waveguide or transmission line)
• low-loss (< 0.5 dB)
• low cross-coupling (< - 40 dB?)
• bandwidth ~ 30%
• mass production? 1024 required, bands from 30 GHz - 300 GHz
• see ClOVER design, Giampaolo Pisano et al.
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CIOVER OMT
• G. Pisano et al.
IEEE Micr. and Wireless Comp. Lett.
17(4) 2007
• electroformed copper
QuickTime™ and a
decompressor
are needed to see this picture.
• WR10 waveguide band (75-110 GHz)
• ms’d return loss -22 dB avg. across band
• ms’d isolation -45 dB avg. across band
• 100’s req’d for ClOVER
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Phase Modulators
• require 2 for each antenna (one per polarization)
• input interfaces to OMT output (w’guide or transmission line)
• ~ 30% bandwidth
• low insertion loss (< 0.5 dB)
• low amplitude modulation
• step through a phase sequence similar to Walsh function
- co-add signals from redundant baselines (Charlassier et al. ‘08)
- # steps minimized by having multiple phase angles
(Hyland, Follin, & Bunn arXiv:0808.2403v1)
• for 8 x 8 array
- steps of 360/15 = 24° is optimal
- sequence length is 675 steps
• switching speed > 100 Hz
• waveguide Ferrite Rotation Modulator (FRM) see B. Keating
• planar modulators (MEMs and SIS) see A. Kogut
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Ferrite phase shifter performance
Gault, Malu, Bierman, Keating, et al.
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Bolometers
• filled arrays required to capture all radiation in focal plane
• # pixels ~ 4 X Nhorns for each interferometer module
• near photon noise limit for
-optical efficiency of ~ 12% ( ~ 50% / 4)
-bandwidth 30%
-CMB background loading
• Backshort Under Grid (BUG) arrays for GISMO (λ = 2 mm)
- increase 64 pixels → 256 pixels
- reduce G
- extend to λ = 1 cm
- $400K/yr for 3 years
• other candidates?
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Adding Interferometer Systems
Complete systems are required to test the concept
MBI-4 ….
MBI/BRAIN
Simulations have just become available this year:
R.A. Watson & L. Piccirillo (poster)
J.-C. Hamilton et al. (2008) ArXiv 0807.0438
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CMBPol Technology Workshop
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Initial simple simulations of Rotman interferometer
(Watson & Piccirillo)
TQU HEALpix map
PSD1 VL-HR
PSD2 VL-VR
PSD3 HL-VL
PSD4 HL-VR
PSD5 HL-HR
PSD6 HR-VR
The simulation was carried on a 4x4 array
shown in figure 4 with a 5o FWHM with a
spacing of 20 wavelengths between
elements using a HEALpix TQU map
generated by synfast using a concordance
model.
The signal from each HEALpix pixel is
traced through all horns through the Rotman
stacks to the detectors where the complex
sum is made and its contribution detector
power determined
Geometry of dual
polarization elements
Correlation pairs for
each PSD lock-in
The lower panels show the real and
imaginary parts of visibilies recovered by
the FFT on the different phase switched
detector stacks.
The stronger unpolarized signals (CMB
fluctuations) can be seen on PSD channels
2, 5 and 7 with weaker polarized U
visibilities at 10% on PSDs 1,3,4 and 6
37
Sky
BRAIN/MBI
10 cm
horns
30 K
First module for
deployment at Dome C,
Antarctica
30 K
phase
shifte
rs
back
horns
60 cm
Workshop at APC, Paris, June ‘08
“Bolometric Interferometry
for the B-mode Search”
40 cm
30 K
10 cm
300 mK
Bolometer array
70 cm
Bolometric Radiation INterferometer
•France
MBI
•United States
–Astroparticule et Cosmologie (APC), Paris
•Brown University
–Centre d’Étude Spatiale de Rayonnements (CESR), Toulouse
–Centre de Spectrométrie Nucléaire et de Spectrométrie de Masse (CSNSM), Orsay •University of Wisconsin,
Madison
–Institut d’Astrophysique Spatiale (IAS), Orsay
•University of Richmond
•Italy
•UC San Diego
•University of Illinois
–Università di Milano - Bicocca
–Università di Roma - La Sapienza
•United Kingdom
•University of Wales, Cardiff
•United Kingdom
•University of Manchester
–University of Manchester
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•NUI Maynooth
–University of Wales - Cardiff
Adding Interferometer Technology Readiness
Technology
corrugated horn antennas (singles)
platelet arrays
smooth-wall horn arrays
OMT (< 100 GHz)
ClOVER OMT (150 GHz?)
phase modulator
- ferrite (2 state, <150 GHz)
- MEMs/SIS (2 state)
beam combiner
- quasi-optical
- guided-wave
focal plane bolometer arrays
- NTD Ge
- Backshort-Under-Grid TES
LHe Cryostat
Sub-K Cooler: Single-shot ADR
27 August 2008
TRL
9
5
3
9
4/5
Heritage
WMAP & COBE
QUIET
TBD
WMAP
ClOVER
5
2/3
BICEP & MBI
PAPPA
5
2
MBI
TBD
8
6
9
9
Planck & Herschel
GISMO
Spitzer, ISO, Herschel, COBE
ASTRO-E2
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Summary
Why interferometry?
Challenges
Beam combination: pairwise vs ‘all-on-one’
Guided-wave beam combiner
Quasi-optical beam combiner
MBI
EPIC Interferometer
Required technologies (bolometric interferometer)
horn antenna arrays
OMTs
phase modulators
beam combiner/correlator
filters
bolometers/readout
100 mK cooler
27 August 2008
CMBPol Technology Workshop
40
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