29 January 2009 1 Intensity Interferometry Workshop
Stellar Intensity Interferometry: The Background
John Davis
Sydney Institute for Astronomy School of Physics University of Sydney NSW, Australia
Stellar Intensity Interferometry: The Background John Davis Sydney - - PowerPoint PPT Presentation
Stellar Intensity Interferometry: The Background John Davis Sydney Institute for Astronomy School of Physics University of Sydney NSW, Australia 29 January 2009 Intensity Interferometry Workshop 1 Personal Notes I regret that I cannot
29 January 2009 1 Intensity Interferometry Workshop
Sydney Institute for Astronomy School of Physics University of Sydney NSW, Australia
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I regret that I cannot make this presentation in person but an outline
radio version of intensity interferometry was implemented
student and then as a Postdoc throughout the development
Stellar Intensity Interferometer and no young postdoc in his right mind would have said anything but “Yes please!”
since.
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and the role of Richard Twiss
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The Origin of the Idea of Intensity Interferometry
and Cassiopeia A, were unknown and some thought they were “radio stars”. Robert Hanbury Brown (RHB) was determined to measure them
a minute of arc and easy to measure with a conventional interferometer but, if they were stars, extremely long baselines would be needed and RHB concluded that this was impossible with the available technology
the radiation from a discrete source in the sky is picked up at two different places on Earth, is there anything besides the phase and amplitude of the signals which we can compare to find the mutual coherence?”
and realised that the noise corresponded to low-frequency fluctuations in the intensity of the signal and convinced himself that the correlation between the intensity fluctuations was a measure of their mutual coherence.
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The Entry of Richard Twiss
idea of intensity interferometry was sound, he was not able to develop the mathematical theory to establish the sensitivity himself
(RQT), a gifted mathematician
no good, it doesn’t work!”
intensity interferometry
the technique and to measure Cygnus A and Cassiopeia A
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The Radio Intensity Interferometer Equipment
Antenna Systems Heterodyne receivers tuned to 125 MHz with Δf of 200 kHz Square-law detectors Low-frequency filters Δf from 1 to 2 kHz Correlator Delay line Radio link
(Hanbury Brown, Jennison, & Das Gupta, Nature, 170, 1061, 1952)
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The Radio Intensity Interferometer Experiment
that would be observed with a Michelson type interferometer
determine the angular dimensions of Cygnus A and Cassiopeia A
(Hanbury Brown, Jennison & Das Gupta, Nature, 170, 1061, 1952)
Cassiopeia A was roughly symmetrical with a diameter of approx. 3.5′
Australia had also measured these sources with conventional radio interferometers and obtained similar results
(Mills, Nature, 170, 1063,1952; Smith, Nature, 170, 1065, 1952)
the sources were clearly not stars – but that is another story
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Lessons from the Radio Intensity Interferometer
than for a conventional amplitude interferometer: the tolerance was set by the maximum frequency of the filtered low-frequency signals whose correlation was being measured, and not by the frequency of the radio signal
in spite of violently scintillating signals due to the ionosphere
perhaps the most astonishing and valuable feature of intensity interferometry – it can work perfectly through a turbulent medium
could be made to work at optical wavelengths and measure the angular diameters of stars
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The Start of Optical Intensity Interferometry
interferometer The radio intensity interferometer The envisioned optical analogue
be correlated at the two photocathodes for coherent incident light
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Optical Intensity Interferometry Laboratory Experiment
superimposed and correlation was observed in close agreement with the theoretical prediction
C1 laterally with the slide, no correlation was observed
(Hanbury Brown & Twiss, Nature, 177, 27, 1956)
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the RHB & RQT results were wrong
Ferguson (Nature, 178, 481, 1956) carried out experiments and did not detect correlation – the latter went as far as stating that the existence of correlation would call for “a major revision of some fundamental concepts of quantum mechanics”
conditions of their experiments . RHB & RQT did the calculations (Nature, 178,1447, 1956) and showed that Adám et al. would have needed to integrate for >1011 years and Brannen & Ferguson for >1000 years to achieve a S/N ratio of 3!
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technique and RHB & RQT showed that they were simply too insensitive to record correlation
Brannen & Ferguson coincidence counting experiment with a brilliant light source of narrow spectral bandwidth They not only measured their predicted correlation but showed that the chance
theory and his analysis of the three experiments came to the same conclusions as RHB & RQT
measure the angular diameter of a main-sequence star (Sirius) to demonstrate the astronomical potential of intensity interferometry
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Simplified diagram of the apparatus The starlight collectors – two World War II 1.56 m diameter searchlights
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the winter of 1955-6 – wet, cold & muddy!
Although the measured angular diameter of 7.1±0.55 mas is larger than the currently accepted value of ~6.0 mas it was a remarkable achievment
(Hanbury Brown & Twiss, Nature, 178, 1046, 1956)
This measurement showed beyond doubt the potential of stellar intensity interferometry and led to the Narrabri Stellar Intensity Interferometer
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Simplified diagram of the Narrabri Stellar Intensity Interferometer (NSII)
Output to printer the correlator (some details later) P1 and P2 are Photomultipliers f1 and f2 are identical wide-band filters
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The Narrabri Stellar Intensity Interferometer (NSII)
The general layout of the NSII
188 m, was chosen to resolve the O5 star ζ Puppis
was kept perpendicular to the star’s direction
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The Narrabri Stellar Intensity Interferometer (NSII)
Stellar Observations (1964-1972)
188 m diameter track Reflectors Catenaries (Signal & power cables) Control Building Reflector Garage Baseline
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used at the centre and the longer radius ones towards the edge of the paraboloids.
Diameter = 6.5 metres 252 individual hexagonal mirrors 251 aligned on the signal detector and 1 on a separate star guidance detector
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JD in control!
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The Analogue Control Desk of the NSII (circa 1967) The Digital Control Desk of SUSI (2008)
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between the fluctuations in the anode currents of the photomultiplier detectors at the foci of the two reflectors
was very small (<1 in 105 for a bright unresolved star)
together and the correlation was a unidirectional output superimposed on random noise
gain drifts, pick up, and cross-coupling. Phase switching techniques were essential to overcome these problems as shown on the next slide
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Block diagram of the correlator
10 second phase switch to minimise the effect of drift in circuits and counter false correlation due to pick up and coupling between circuits 5 kHz phase switch to counter stability problem of high gain DC ampllifiers
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The output printer Originally all thermionic valves – transistors were not an option in 1961!
Note the size!
Transistorised sequence timer that replaced a mechanical/microswitch system circa 1965
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by the observer as shown in the example below for 20th May 1965 for
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by the observer as shown in the example below for 20th May 1965 for
Number of 100 second integration cycles
“Dummy” run β Cru: 32.7m β Cru: 94.2m “Dummy” run
“Dummy” Runs Between observations the detectors were exposed to the same light levels as from the star using incoherent artificial sources to monitor any drift in the system Correlation
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Calibrated with a standard source of wide band noise fed simultaneously into both channels in place of the photomultiplier
and the scale changes if, for example, the detectors are changed
with the same instrument parameters – also identifies binaries
be taken into account as we did
reducing all results to a consistent scale was a tedious exercise
to using calibration sources, as is done for amplitude interferometry
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to F8 resulting in the effective temperature scale for early-type stars
(Hanbury Brown, Davis & Allen, MNRAS, 167, 121, 1974; Code, Davis, Bless & Hanbury Brown, ApJ, 203, 417, 1976)
spectroscopic binary (α Vir) (Herbison-Evans et al., MNRAS, 151, 161, 1971)
Rayet star γ2 Vel in ionised carbon lines
significant results for the last three experiments but they illustrated the potential of high angular resolution stellar interferometry
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The Hiatus at the Conclusion of the NSII Programme
would not have added significantly to the results already obtained
capabilities of the new detectors that were being developed at that time - but I persuaded him that we should build on our experience and develop a Very Large Stellar Intensity Interferometer (VLSII)
do, including measuring the pulsations of Cepheids, and concluded that we would need to reach a visual magnitude of >+7
with the CfA to detect atmospheric Cerenkov light from extensive air showers (Grindlay et al., ApJ, 197, L9, 1975; Grindlay et al., ApJ, 201, 82, 1975)
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S/N ∝ A.α √ Δf.N
at our disposal – the latter limited by crude optics
were interested in, we developed a proposal for a Very Large Stellar Intensity Interferometer (VLSII)
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based, in part, on predictions by RCA about future photomultipliers and
N was based on a study of polarising and dichroic beamsplitters and was limited by the crude optics
specifications of the latter were set by the maximum funds we estimated might be achievable. Parameter NSII Optimistic VLSII A (m2) 30 160 Δf (MHz) 80 1000 N 1 10 α (%) 25 30 Gain 1 72 mlimit +2.5 +7.1
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The basic configuration of the proposed VLSII
Aligned to observe a star in the zenith Aligned to observe a star at ~70o elevation
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in each arm
foci of fixed paraboloids
JD and RHB with the model of the VLSII
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sensitivity to represent more realistically what we believed could be achieved in practice within a reasonable timescale
A limiting magnitude of +5.8 did not meet our needs Parameter NSII Optimistic Realistic VLSII VLSII A (m2) 30 160 160 Δf (MHz) 80 1000 200 N 1 10 6 α (%) 25 30 25 Gain 1 72 21 mlimit +2.5 +7.1 +5.8
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meet our needs
interferometer might be more sensitive and I persuaded RHB that we should make a comparison of the two techniques
been developing a small scale modern Michelson interferometer in Italy (I had worked on an early version with RQT in England during a sabbatical)
promised greater sensitivity and we decided to abandon the VLSII and RHB left me to develop a prototype modern amplitude interferometer
to reach the sensitivity we were after!
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The Sydney University Stellar Interferometer 12.4 m Prototype
150 mm diameter southern siderostat & relay mirrors. (The northern siderostat is hidden by the building)
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The Sydney University Stellar Interferometer 12.4 m Prototype
needed for a large long-baseline amplitude interferometer
boundaries of technology and some aspects were only just possible
measurement of the angular diameter of Sirius that was in good agreement with the NSII value but achieved in a fraction of the
path length compensation, and rapid signal sampling & processing
the Sydney University Stellar Interferometer (SUSI)
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The Sydney University Stellar Interferometer (SUSI)
Seen from the northern end of its 640 m North-South baseline array
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An input station & siderostat Optical Path Length Compensator Blue beam combination system Red beam combination system
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The following beam-combination systems have been used for the scientific programme to date but are in the process of being replaced: SUSI is being upgraded for remote operation with a new beam-combination system (PAVO) developed in a collaboration for both SUSI and CHARA
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systems
(in spectroscopic binaries)
combination with spectroscopic radial velocities, determination of distances and mean radii of Cepheids
to determine the mass of a single star
Some Highlights of the SUSI Science Programme
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been considered by others
1. What science is possible with II that cannot be done with AI? 2. What is the sensitivity limit for a modern Intensity Interferometer and how does it compare with current Amplitude Interferometers? 3. Methods of calibrating measurements of correlation
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Some possible stellar programmes:
All these programmes have been, and are being addressed by current amplitude interferometers and I do not see where II could make a significant contribution
An often quoted advantage of II is that the problems were solved with the NSII and that there are no unknowns Although it has taken a long time to achieve, I believe that the same can now be said of AI First, a comment:
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There are non-stellar programmes that may be possible with II but not with AI – I have not had time to study these possibilities but they must be carefully evaluated taking into account what is possible with current and future amplitude interferometers It has been suggested that AI cannot operate at the short wavelengths and long baselines needed for the hottest stars because of increasing seeing effects. I do not believe this is true for the following reasons:
technique.
easily reached Blimit +7 - even with the small SUSI beam diameter.
beyond that (Davis et al., MNRAS, 273, L53, 1995)
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2. What is the sensitivity limit for a modern II and how does it compare with current AIs?
uncertain factors entering the calculations if the large light collectors developed for very high energy gamma-ray observations are to be used, including:
noise, reducing mlimit
reflectors must be good enough for II
path lengths and hence limit the bandwidth that can be used
sensitivity calculations but it would appear that with existing arrays, the limiting magnitude would be in the range +6 to +8
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a much fainter mlimit, but would be hard to fund in the face of the achievements of AI, unless a compelling scientific case could be made A summary of selected long-baseline optical/IR amplitude interferometers
Acronym Location Number Aperture Maximum Wavelength Instrument Limiting Notes Status
Diameter Baseline Range Magnitude * Apertures (m) (m) (mm) SUSI Narrabri, Australia 2 0.14 640 0.43-0.53 Blue system B ~+2.5 Superseded W 0.53-0.95 Red system R ~+5 Superseded W 0.6-0.9 PAVO R ~ +7 C ISI
2 1.65 70 10
W NPOI Flagstaff, USA 6 (4) 0.12 (0.35) 437 (38) 0.45-0.85
W CHARA Mt. Wilson, USA 6 1.0 330 0.45-2.4 Several other W 0.4-0.9 VEGA R ~ +8 instruments W 0.62-0.9 PAVO R ~ +10
W Keck Mauna Kea, Hawaii 2 (4) 10 80 2.2-10
Only 1 baseline W VLTI Cerro Paranal, Chile 4 (4) 8 (1.8) 130 (200) 1.0-10 MIDI (8m) N ~+4 W MIDI (1.8m) N ~+0.7 W AMBER (8m) H & K ~ +7
W AMBER (1.8m) H & K ~ +5 with PRIMA tracking W PRIMA K ~ +8-+11 C MRO New Mexico, USA 6 (+4) 1.4 340 0.6-2.4
Imaging B # Spectral band not given * W = Working; C = Commissioning; B = Being built
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magnitudes of +7 and fainter are being achieved by several instruments including imaging
but are feasible
Acronym Location Number Aperture Maximum Wavelength Instrument Limiting Notes Status
Diameter Baseline Range Magnitude * Apertures (m) (m) (mm) SUSI Narrabri, Australia 2 0.14 640 0.43-0.53 Blue system B ~+2.5 Superseded W 0.53-0.95 Red system R ~+5 Superseded W 0.6-0.9 PAVO R ~ +7 C ISI
2 1.65 70 10
W NPOI Flagstaff, USA 6 (4) 0.12 (0.35) 437 (38) 0.45-0.85
W CHARA Mt. Wilson, USA 6 1.0 330 0.45-2.4 Several other W 0.4-0.9 VEGA R ~ +8 instruments W 0.62-0.9 PAVO R ~ +10
W Keck Mauna Kea, Hawaii 2 (4) 10 80 2.2-10
Only 1 baseline W VLTI Cerro Paranal, Chile 4 (4) 8 (1.8) 130 (200) 1.0-10 MIDI (8m) N ~+4 W MIDI (1.8m) N ~+0.7 W AMBER (8m) H & K ~ +7
W AMBER (1.8m) H & K ~ +5 with PRIMA tracking W PRIMA K ~ +8-+11 C MRO New Mexico, USA 6 (+4) 1.4 340 0.6-2.4
Imaging B # Spectral band not given * W = Working; C = Commissioning; B = Being built
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3. Methods of calibrating measurements of correlation
reflector and measure the correlation between the signals – corresponding to zero baseline. This would lose a factor of 2 in S/N.
target with observations of calibrators - sources of relatively small angular size or of known angular size In all cases the effects of partial resolution by the large reflectors would need to be taken into account
and fit the expected transform. Provided no changes are made to the instrument the zero baseline correlation value can be established for single stars and used to detect binary systems etc.
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stellar studies
achieve greater sensitivity than amplitude interferometers that exist or, in the case of the MRO, are under construction
existing longer baselines (up to 640 m) of SUSI are brought on line, SUSI-PAVO will be capable of measuring some of the hottest stars
achieving the sensitivity for programmes that it can do and that AI cannot The following are my personal conclusions - but I don’t expect everyone to agree with them!
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