Astronomical Requirements for the Millimeter Array Correlator
Michael P. Rupen
National Radio Astronomy Observatory
Socorro, NM 87801
Debra S. Shepherd
California Institute of Technology
Department of Astronomy
Pasadena, CA 91125
&
M.C.H. Wright
Radio Astronomy Laboratory
University of California
Berkeley, CA 94720
February 1998
Taking full advantage of the sensitivity and flexibility of the Millimeter
Array (MMA) will require an impressive correlator. The signals from
40 telescopes (possibly as many as 128, if major foreign collaborations
materialize) must be correlated over bandwidths of at
least 2 GHz, and preferably 8 GHz, per polarization, producing
of (bandwidth times polarizations). This should be split amongst at least 4,
and preferably 8, independently-tunable baseband pairs. There should
be 500-1000 channels (with two polarization products each) over the full
8 GHz, and one should be able to trade bandwidth for channels in a fairly
flexible way. Standard
sustainable integration times of 0.1 second are required, with sustainable
integration times of
being highly
desirable. This gives a required sustainable data rate of at least
250 million visibilities per second. The spectral dynamic range,
measured either as the accuracy of continuum subtraction or the ratio of
the peak to the spectral sidelobes of a narrow signal,
must be
.
The prospect of a collaborative
project with international partners leaves several of the most important
correlator requirements uncertain.
This memorandum aims to set forth the astronomical requirements for the correlator of the proposed Millimeter Array (MMA). The current working design for that correlator is described in MMA Memorandum 166 (Escoffier 1997) and MMA Memorandum 194 (Rupen & Escoffier 1998), the latter of which also discusses the limits on the expansion of that design. Here we step back to ask what astronomers would like to be able to do with the instrument, and what requirements those desires set for the correlator. The emphasis is naturally on the more challenging projects, those which push the correlator to its limits; at the same time we try to specify a reasonable minimal as well as the ``dream'' correlator. The underlying philosophy is that the correlator should not rule out plausible experiments which would otherwise be allowed by the design. Obviously not all of these experiments will be doable when the MMA first opens; but if the VLA experience is any guide, the original correlator will remain in use for many decades following first light.
To avoid confusing what is intended primarily as a scientific discussion, and to restrict the length of an already-lengthy document, we defer consideration of cost equations and other practical matters of correlator design to a later memorandum. Similarly, we do not here compare the requested to the current design specifications.
We use the same terminology as MMA Memo 194. The numbers given here are for reference only, to make a somewhat confusing discussion more concrete, and are based on the current notional design of the MMA system.
We assume throughout that the MMA will eventually observe through all
atmospheric windows between
GHz and
GHz, although it will
probably not be equipped with all of the requisite receivers initially.
For concreteness we also assume that linear polarizations (X and Y) are
recorded.
The lower limit to the number of antennas is set by the desire for excellent `snapshot' uv-coverage. Snapshot observations are of more importance to the MMA than to other interferometers for several reasons. First, the atmosphere at millimeter and submillimeter wavelengths is highly variable both in opacity and in phase coherence, and one wishes both to take advantage of brief periods of exceptionally fine weather, and to image large regions on the sky rapidly to minimize systematic effects across the resulting maps. This becomes progressively more important at higher frequencies. Second, the MMA's excellent sensitivity makes very short observations attractive, if the instantaneous uv-coverage is good enough to ensure accurate images. Finally, mosaics are expected to become rather common with the MMA, given the small primary beams at these frequencies; the quality of those mosaics will be set in part by the consistency and completeness of the uv-coverage of each pointing. The second and third of these points were quantified in Cornwell, Holdaway, and Uson (1993) and further elaborated in a series of MMA memoranda by Holdaway and others (Holdaway 1990, 1992; Holdaway & Foster 1994; Wright 1997). All three desiderata considered together led to the design goal of 40 antennas for the MMA (cf. the original MMA proposal to the NSF [1990]).
Another, less strong argument for a large number of antennas is the desire for multiple subarrays, each with very good mapping capabilities. This is discussed further below (§3.7).
More significant are the recent discussions between NRAO, ESO, and Japan's
NAO concerning possible partnership(s),
which would result in a much larger array. The most recent
European proposal (Downes et al. 1997b) suggests
dishes, set by the desire to maximize collecting area while minimizing the
number of antennas, subject to the constraint that the antennas maintain
excellent performance for mosaicing and for high frequency work. The
complexity of the correlator itself, and the resulting data rates, are the
main arguments for minimizing the number of dishes. On the other hand, it is
clearly easier to build superb small dishes than superb big ones, and
alternative suggestions range from
to
dishes. Since we will probably not know until at
least the end of 1999 whether ESO and/or NAO will actually fund the
proposed joint project, the number of telescopes could be a factor two lower
than suggested here. So the bottom line is that the MMA correlator should be
able to handle at least 40 antennas, and perhaps as many as 80-128 if these
major foreign partnerships materialize.
Unfortunately the number of antennas is not something that can readily be changed in the correlator at some later date; see MMA Memo 194. If we are to have e.g. 80 telescopes eventually it is far preferable to design the correlator to handle them from the start. Of course a correlator which can handle more telescopes than are actually built would allow the addition of further dishes after the completion of the original project (cf. Downes et al. 1997b).
Many observations will benefit from the widest possible bandwidths. For continuum experiments this is important mainly for sensitivity, and so will directly affect virtually all such observations. Projects for which sensitivity is paramount, even for the ``maximal'' combined US and European array, cover every area of millimeter astronomy: the detection of proto-Jupiters in other solar systems; high-resolution dust mapping around young stellar objects (YSOs); the observation of pulsar emission at wavelengths which minimize the effects of dispersion; the search for dust emission in high-redshift galaxies and proto-galaxies; and so on and on. Sensitivity becomes progressively more important at higher frequencies, as the atmospheric contribution leads to higher and higher system temperatures; and at higher resolutions, since the same total flux is spread over a larger number of synthesized beams. Some of the most interesting science expected to come from the MMA depends on high-resolution, low-noise images. The importance of wide bandwidths in achieving the desired sensitivity cannot be stressed enough.
Wide-band continuum observations will also provide accurate
single-band ``colours'' (spectral indices). While a few narrow basebands
spread across the band might suffice for bright sources (the Sun, the planets,
Sgr A
, M87), wider bandwidth (e.g., 1 GHz) `chunks' spread over a
receiver's frequency window would allow similar analysis of more standard
sources, in particular the measurement of thermal dust temperatures in
Galactic YSOs and extragalactic disks.
The above argues for a wide continuum bandwidth using dual polarization for sensitivity. Full polarization imaging is also important, primarily for stellar emission, dust polarization mapping, Faraday rotation observations, and planetary work (where the polarization fraction is of order 1%). The signals are expected to be quite faint, but the results will be well worth the effort, particularly in mapping the magnetic fields in molecular clouds and accretion disks.
A number of spectral line experiments also require or benefit from wide bandwidths.
In sum, a bandwidth of 2 GHz, producing two correlator polarization
products (XX & YY), is necessary for a wide variety of spectral line
experiments. Observations of pressure-broadened planetary lines and radio
recombination lines associated with the Sun or AGNs require double that
bandwidth (4 GHz with two polarization products) to fit the line into a single
frequency setting, while the very broadest of such lines at the highest
frequencies might require up to 5 GHz. For continuum observations sensitivity
demands the widest bandwidths possible. A large number of experiments would
also benefit from the ability to sacrifice polarization products for
bandwidth; most experiments not involving linear polarization measurements
would prefer to cover, e.g., 16 GHz producing only the parallel-hand (XX,
YY) polarization products, to always getting full Stokes information but
only over 8 GHz. In any event the correlator should match the rest of the
instrument in allowing the maximum bandwidth permitted through the receivers,
backends, etc; with the current systems design, with
sent to the
correlator from each antenna, this would imply all four polarization
products for an 8 GHz bandwidth.
The highest frequency resolution needed for the MMA is set by the
possibility of future millimetric bistatic radar observations of solar system
objects, which would require a few hundred
channels. Apart
from this the highest velocity resolution required is
(2-5 kHz at 30 GHz), needed for a wide variety of
experiments: measuring wind velocities on Venus; sampling thermal and/or
dynamical line widths of comets, planetary satellites, protostellar disks,
and dark cloud cores; finding and characterizing the structure of narrow
absorption lines; and measuring magnetic field strengths via Zeeman
splitting (of order 1 Hz splitting per microGauss). SETI observations would
benefit from 1 Hz or even finer resolution (J. Tarter 1997, priv. comm.),
but this should not be allowed to drive the correlator
design.1
At the other end of the scale, very wide channels are desirable primarily to reduce the data rate and the total data volume produced by an experiment. Most continuum observers would be happy with as few as one channel per baseband pair, corresponding (in the current design) to 1-2 GHz channels. However, there are a number of constraints on how wide a channel is actually usable:
This suggests that the broadest practicable channels will be
wide. Of course for a lag correlator this number is not very important
for the design.
Finally, between these two extremes one must be able to choose frequency resolution (and bandwidth) in geometric (factor two or whatever is convenient) intervals; preferably these choices could be made independently for each baseband or baseband pair.
There are two main arguments for having as many baseband pairs as possible. First, to the extent that each baseband may be positioned independently in frequency, more basebands imply more flexibility in observing several lines or several `chunks' of continuum within a single band. Second, to zeroth order the size of a lag correlator goes inversely as the number of basebands, since one can use proportionately fewer lags to cover the same total bandwidth with a given frequency resolution (see e.g. MMA Memo 194). Of course there are counter-arguments which suggest a smaller number of basebands. Astronomically, it is difficult to keep consistent calibration between different basebands, particularly for single-dish data; this implies that the maximum bandwidth of a baseband should roughly match the width of the broadest lines that would regularly be observed. From considerations like those in §3.2 above, this probably corresponds to 1-2 GHz per baseband. Practically, correlators with many basebands (e.g., the analogue correlator at the 12m) have not been terribly successful, and the ideal number of basebands from an engineering point of view is a subject of current debate. That debate however is outside the scope of the present paper, which purports to concentrate on astronomical needs, and the remainder of this subsection is addressed to the question of how many independently-tunable basebands are necessary to allow the observer to take good advantage of the capabilities of the MMA.
For continuum work one wants a number of baseband pairs for two reasons: first, to allow one to position individual `chunks' of continuum bandwidth to avoid strong lines, atmospheric contamination, and strong interference; and second, to allow single-band spectral index (or colour temperature) mapping. Four independently-tunable baseband pairs is probably the maximum necessary for these sorts of experiments. Note that each BB pair will be made up of a number of channels (see the next section), so while one would want to avoid broad interfering lines, narrow ones are not a problem, since the contaminating lines can simply be deleted from the data set.
Line experiments in general benefit from having as many BB pairs as possible, as this maximizes the observing efficiency by allowing many lines (as well as the continuum) to be observed at once. This is particularly important at high frequencies and for the larger array configurations, since one wishes to take the best advantage of periods of good phase stability, low wind conditions, and/or low opacity. For similar reasons very long integrations, which may be quite common (Evans et al. 1995), should also be carried out simultaneously in as many lines as possible. That many interesting lines are available is very clear; for instance, Schilke et al. (1997) found an average of 26 reasonably strong lines per GHz in the 350 GHz window towards Orion K-L. Obvious choices for multi-line studies include a set of different isotopes and transitions of a single molecule, which could easily add up to 8 or more lines in a single band. Many experiments require, or would benefit greatly from, simultaneous wide and narrow bandwidths; measuring accurate line-to-continuum ratios, referencing the phase of a line to a strong continuum or vice versa, observing a single line at multiple velocity resolutions (e.g., observing both a protostellar disk and the associated outflow at the same time), and `piggy-back' surveys (e.g., doing a pencil-beam survey for CO while mapping the emission in a nearby galaxy) are all examples of observations of this type.
Finally, VLBI observations using the MMA would benefit from having the same flexibility as the VLBA system provides, i.e. 8 independently-tunable basebands.
Based on the above considerations, the ideal correlator would allow for a minimum of 4 BB pairs, and preferably 8. Note that this is one of the aspects of the correlator which is modular - it would be relatively easy to add more basebands later (MMA Memo 194). At least one of these BB pairs should have a maximum bandwidth of at least 1-2 GHz, and together they should of course span the full bandwidth discussed in §3.2. Insofar as possible, since even broader lines will be observed occasionally, and perforce be split amongst several basebands, one should be able to join these basebands together smoothly over frequency, with little loss in sensitivity and minimal systematic errors. The bandwidth and channelization of each baseband (or, at a minimum, each baseband pair) should be set independently, allowing e.g. one BB pair to cover 1 GHz with 100 channels while another covers 10 MHz with 1000 channels.
Multibeam feeds, if used, would represent an additional complication, as presumably one would want to correlate all the beams from one telescope with the corresponding beams from all others. To first order this would be similar to having additional (sets of) BBs. This should probably not drive the initial correlator design.
A number of experiments benefit from a large number of channels; many of these involve wide (several GHz) total bandwidths. Among the most obvious are:
Apart from line surveys and the like (most of which would benefit from as many as 1000 channels per GHz), and assuming that one can trade bandwidth for channels in a fairly flexible fashion, all of these experiments correspond to having 500-1000 channels spread over 8 GHz. Since most of these projects are limited by sensitivity, dual polarization is essential. Only Zeeman splitting and maser observations would benefit from both the maximum number of channels and full polarization products, and we could probably get by with only half as many channels when asking for full polarization information. Line surveys of course could use as many channels spread over as wide a bandwidth as is practicable, but they should probably not drive the correlator design. It seems unlikely that any reasonable experiment would demand many more channels over a narrower bandwidth; although the sensitivity of the instrument would support this, the intrinsic linewidths are broad enough that much higher resolution does not seem necessary. The obvious exception would be SETI searches, which benefit from very high resolution over the broadest possible bandwidth; again this should probably not be allowed to drive the correlator design, though it should be allowed if it is not terribly costly.
We note that Escoffier's current (1997) correlator design would give 512 channels over an 8 GHz bandwidth for each of two polarization products (e.g., XX & YY) (see MMA Memo 194), nicely matching the above (independently derived) astronomical specification.
The shortest astronomically interesting integration period for the MMA is the subject of a lengthy discussion in MMA Memorandum 192 (Rupen 1997b). The conclusions of that memo were:
On the other end of the scale, the enormous data rate coming from an instrument with at least 40 telescopes and several thousand spectral channels argues for the availability of much longer integrations, up to perhaps some 10s of seconds or longer. The limit here will be the phase wind due to the electronics and the atmosphere, which (at the higher frequencies) may often be so fast that long integrations would require on-line phase correction, which would add significantly to the complexity of the correlator. At low frequencies (30 GHz) integrations of 30 seconds or longer will often be fine. This is discussed further in §3.9.
Subarrays will be much more important for the MMA than for the VLA or other existing interferometers, for a wide variety of reasons.
Total power measurements will be much more important than for centimeter interferometers, and require higher accuracy. Mostly this is because the primary beam will be small, and many sources will require mosaicing; single-dish observations will be needed to fill in the central hole in the uv-plane. There are various arguments that the MMA itself should provide its own short-spacing information, rather than relying on other dishes as most current interferometers do. The MMA will be the premiere millimeter telescope in the world, and as such is expected to be observing almost continuously, with high sensitivity, covering large areas of the sky. The corresponding single-dish measurements will have to match the MMA observations in both quantity and quality, over the entire spectral window covered by the MMA. It would be unreasonable to rely on any other instrument for this sort of vital support; nor are there any international, publicly-available instruments capable of providing it. Further, a series of studies (e.g., Emerson 1990) have shown that the MMA telescopes themselves can be used quite handily to fill in the missing short spacings, without any need for larger dishes. Finally, there is a software/post-processing advantage to having a `standard' source for total power data, rather than allowing for a wide variety of possible instruments; one could optimize the (automatic?) routines for mosaicing and the like, for the case of MMA single-dish data.
The correlator must therefore be prepared to handle total power measurements from all MMA dishes simultaneously,2 or at least from all dishes equipped to produce such data.3 The single-dish data should be allowed at least the same number of channels, bandwidths, etc. as provided for the interferometric data. A number of special observing modes must be supported as well:
Although it would seem easiest to use the same correlator for the auto- and the cross-correlations, there is no strong reason that the same correlator must handle both.
Finally, one must distinguish between spectroscopy and continuum total power data.4 One may well want to do both at the same time (usually to be able to subtract the line emission from the continuum), but they are quite different things. One does single dish spectroscopy with the usual autocorrelations, with level controls etc. used in the same way as one does for interferometry; but this may either destroy or severely injure the absolute amplitudes used for continuum measurements. The current plan is to do continuum single dish measurements based on detectors located in the antennas, far ahead of all the stuff that might bother the gain stability. This detector system would then be well outside the correlator.
Operating at very high frequencies requires monitoring the atmosphere
on short timescales. There are two issues: correcting the amplitudes for
atmospheric opacity fluctuations, and maintaining phase coherence. Based
on the extensive site testing database and atmospheric transmission models,
Holdaway (1998; in prep.) concludes that short timescale (i.e., 30 seconds)
amplitude fluctuations will typically be only a few percent rms at 650 GHz.
On longer time scales (600 seconds) amplitude fluctuations rise to about
10% rms at 650 GHz. This implies that opacity corrections need only be
calibrated out on time scales of 30 seconds or longer. Similar modelling
gives atmospheric coherence times at 650 GHz of
seconds for median
weather conditions and 90% coherence (<1 second for 98% coherence),
rising to longer than 10 seconds (90% coherence; about 3 seconds for 98%\
coherence) during the best 20% of the weather, which is presumably when
most high-frequency work will be carried out. There is thus little need
to make phase corrections on time scales less than about a second. Other
simple arguments give similar time scales. For instance, assuming peak wind
speeds aloft of 10 m/s, a given atmospheric perturbation will cross an
antenna in
; it seems unlikely that one
will be able to sensibly correct phases any faster than that. It is also
questionable whether one could measure the phase any more frequently than
this.
So, at the highest frequencies one might want to correct the phase every second or so, and the amplitude every 30 seconds. This implies that all statistics related to the atmospheric phase - radiometric measurements of the water line, opacities, wind velocities, temperatures, on-site water vapor measurements, pressure - together with pointing information, must be written out with the data, on that timescale.5 This basically increases the size of the output data set and the corresponding data volume, without requiring much of the correlator. However, integrations which are longer than about a second at high frequencies may require on-line corrections to the phase,6 to avoid decorrelation within an integration period. This is a major issue, because such corrections may be complicated, and because long integrations would be very helpful in reducing both the data rate and the total volume of data which has to be stored on disk and eventually analyzed. Such on-line corrections would make the correlator significantly more complicated. One option would be to have the correlator always produce a data stream with a maximum integration time of one second, and allocate a special-purpose processor to do the corrections and average the data in time after the correlation. Unfortunately that processor would have itself to be fairly complex. This is an area which needs further study fairly quickly.
The term ``spectral dynamic range'' (SDR) is used to mean at least three different things:
The MMA, especially in the larger versions suggested for the collaboration
with the Europeans, will be a very sensitive instrument, with noise levels at
230 GHz in one minute as low as
in the continuum and
(
, for the smallest configuration) in a 0.2 km/s
channel. One will often be looking for weak signals in the presence of
strong confusing sources, either continuum or line (e.g., masers), requiring
a high SDR potentially in all three senses.
Although it is not clear how to relate image quality to the correlator design, for completeness it may be worth mentioning the dynamic range (peak to off-source rms noise level) MMA images will achieve. With noise levels as in the last section and taking 10 hours as a reasonable long integration, one expects dynamic ranges of
Another kind of dynamic range relates to the total range of data within
a single uv-data set - the ratio of the peak short-spacing flux to the rms
noise on the longest baseline. This is in some ways a more difficult
number to derive, since it involves comparing the integrated flux density of
a source to the rms noise in an integration period. Probably the brightest
sources for which one might achieve thermal noise on the longest baselines
are the planets, with brightness temperatures of 200-300 K (for Jupiter and
Venus). The flux density measured on the shortest baseline would then be
of order
where
is the telescope diameter. With a noise level between 5 and
20 mJy on a single baseline in 1 second for frequencies up to about 230 GHz,
the peak ratio of flux density on the shortest baseline to rms noise on the
longest baseline would be of order
.
Although radio frequency interference (RFI) has not in the past been much
of a problem for millimeter interferometers, RFI has been increasing even at
the high frequencies used by the MMA, and will certainly be an issue for at
least the lower observing bands by the time it is built. Currently the main
frequency allocations above 30 GHz have been to satellites, with a few
areas in Q band going to stratospheric balloons and automobile radar
systems. Little
use has yet been made of the frequency space already allocated, but
some important features are already clear. First, most services proposing
to operate at these high frequencies do so because they need fairly wide
bandwidths. This implies that typical RFI signals will be at least a few MHz
wide. Second, at millimeter wavelengths it is more difficult to
generate high transmitter power, while high gain beams require only small
antennas. Thus one would expect most transmissions to be highly beamed at
specific areas. Most importantly, the sidelobe levels of radio astronomy
antennas are likely to have similar gain to those at centimeter
wavelengths, i.e. of order 10 dB for those near the main beam and order
0.1 dB at angles greater than about 50 degrees from the main beam. Since
the collecting area for a given gain is proportional to wavelength
squared, the sidelobe sensitivity to interference decreases with
increasing frequency.7 This leads to the third point, that the bulk of the worrisome
interference will come from satellite downlinks. Since those satellites are
likely to surround the globe, we will not escape their transmissions however
remote the observatory site.
If the satellite downlinks use time multiplexing like IRIDIUM,
they will transmit in brief bursts (IRIDIUM uses 4.5 msec packets) which we
may be able to flag if the signal can be recognized and discarded on
timescales. Such time-sharing may not be very common however,
since most satellite allocations are designated specifically as
space-to-Earth or Earth-to-space, whereas IRIDIUM takes advantage of an
unusual secondary uplink allocation within a primary downlink band.
While the RFI situation is currently fairly benign, we cannot afford to be
complacent. At the VLA the bulk of the interference above
is internally generated, due mostly to the LO systems (the 100-200 MHz
`birdies'). This should be avoided if at all possible at the MMA; it will
do us little good to have clear skies if we bring with us our own headlights.
Further, although no allocations have yet been made above 300 GHz,
those are to be discussed in the 1999 World Radiocommunications Conference.
In addition to the major requirements discussed above, the correlator must allow for a number of more specific constraints:
From the above discussion, the main requirements for the MMA correlator are as follows:
As the astute reader will have noticed, several areas of these correlator specifications would benefit from more careful study. While the need for ancillary data (§3.9) is obvious, whether it would be useful to apply any calibration derived therefrom on-line is not. Although doing this in the correlator would significantly complicate the design, the prospect of averaging down the data before writing them out is very attractive. Perhaps one could employ an intermediate, real-time processor directly after correlation to do some simple calibration and flagging before the data are written to disk. Similarly the maximum channel width is important in limiting the output rate, but will be determined by the accuracy of the delay settings and the frequency characteristics of the LO and related systems.
By far the largest source of uncertainty however is the possibility of significant foreign partners. If either the European LSA or the Japanese LMSA does in fact merge with the MMA, the budget will grow considerably, and a rather different instrument will result. This uncertainty is reflected in several areas of the correlator specifications. The most obvious is the number of antennas, which might go from 40 to a hundred or more. This together with the larger collecting area leads to a desire for more subarrays and more stringent dynamic range limits. Larger antennas have smaller primary beams, which make one want shorter integrations to allow mapping a given sky area in the same total time. Some of the joint proposals, particularly the Japanese, also push for longer baselines.
The MMA correlator will be an impressive and complex instrument. Assuming
100 MHz channels and 1 second integrations, the minimum data rate for a
full-bandwidth, 8 GHz continuum experiment will be
visibilities per second.
For an 8000-channel line observation using 0.1 second integrations this
jumps up by a factor of 1000. By contrast the VLA produces at most
3,300 visibilities per second, the VLBA about 3.3 million.10 A standard
figure of merit (or at least size!) for a correlator is the number of
multiplications per second, computed as
. Using the requirements given above, the
proposed MMA weighs in at
multiplies per second, compared to
for the current VLA,
and
for the VLBA and the GBT.
The MMA will be a great leap forward for millimeter astronomy, much as the VLA was for radio astronomy in the '70s. Almost 30 years later the VLA is limited primarily by its original correlator, which both restricts the total bandwidth and severely constrains the number of channels one can use to cover that bandwidth. Unless the budgetary process changes significantly we can expect the initial MMA correlator to be similarly long-lived. We are designing this instrument therefore not for the 1990s, nor yet for first light in 2005 or beyond, but for the maturity of the instrument 40 years hence. What seems ambitious now may by then seem merely prudent.
We are very grateful to the many people who carefully reviewed this document, to wit: Tim Bastian, John Benson, Bryan Butler, Barry Clark, Larry D'Addario, Ray Escoffier, and Craig Walker. In addition, Dan Merteley and Greg Taylor commented on the RFI discussion, as Chris Carilli did on the sections on calibration. Finally, Ray Escoffier was infinitely patient and helpful in answering a huge number of MPR's questions about correlators.
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Those of the following which were not cited explicitly are useful references either on millimeter array science in general, or on correlator design issues in particular.
Cernicharo, J. & Reipurth, B. 1996, ApJ (Letters) 460, L57.
Churchwell, E. et al. 1997, MMA Advisory Committee Report, November 1997.
Clark, B.G. 1992, MMA Memo No. 85: Some Remarks on MMA System Design.
Cornwell, T.J., Holdaway, M.A., and Uson, J.M. 1993, A& A 271, 697.
D'Addario, L.R. 1989, MMA Memo No. 55: Millimeter Array Correlator Cost Equation.
D'Addario, L.R. 1989, MMA Memo No. 56: Millimeter Array Correlator: Further Design Details.
Dayal, A. & Bieging, J.H. 1995, ApJ 439, 996.
Dowd, A. 1991, MMA Memo No. 66: MMA Correlator: Some Design Considerations.
Downes, D. et al. 1997a, MMA/LSA Proposal from the European Science Group.
Downes, D. et al. 1997b, Recommendation to the MMA/LSA Management Board.
Emerson, D.T. 1990, MMA Memo No. 62: An Independent Simulation of Imaging Characteristics of a Millimetre Array, with and without a single Large Element and an LE pointing correction algorithm.
Escoffier, R. 1995, MMA Memo No. 146: An MMA Lag Correlator Design.
Escoffier, R. 1997, MMA Memo No. 166: The MMA Correlator.
Evans, N. et al. 1995, Report of the MMA Science Workshop.
van Gorkom, J.H., Knapp, G.R., Ekers, R.D., Ekers, D.D., Laing, R.A., & Polk, K.S. 1989, AJ 97, 708.
Gurwell, M.A. 1996, Ph.D. thesis at the California Institute of Technology.
Hogerheijde, M.R., van Langevelde, H.J., Mundy, L.G., Blake, G.A., & van Dishoeck, E.F. 1997, ApJ (Letters) 490, L99.
Holdaway, M.A. 1990, MMA Memo No. 61: Imaging Characteristics of a Homogeneous Millimeter Array.
Holdaway, M.A. 1992, MMA Memo No. 73: Mosaicing with Even Higher Dynamic Range.
Holdaway, M.A. & Foster, S.M. 1994, MMA Memo No. 122: On-the-Fly Mosaicing.
Holdaway, M.A. & Rupen, M.P. 1995, MMA Memo No. 128: Sensitivity of the MMA in Wide-Field Imaging.
Kramer, N., Jessner, A., Doroshenko, O., and Wielebinski, R. 1997, ApJ, in press.
The Millimeter Array (Proposal to the National Science Foundation) 1990.
Olmi, L., Cesaroni, R., Neri, R., & Walmsley, C.M. 1996, A& A 315, 565.
Rupen, M.P. 1997a, VLA Upgrade Memo No. 8: Astronomical Requirements for the New VLA Correlator.
Rupen, M.P. 1997b, MMA Memo No. 192: The Astronomical Case for Short Integration Times on the Millimeter Array.
Rupen, M.P. & Escoffier, R. 1998, MMA Memo No. 194: Astronomical Capabilities of the Current Design for the Millimeter Array Correlator.
Schilke, P., Groesbeck, T.D., Blake, G.A., & Phillips, T.G. 1997, ApJS 108, 301: A Line Survey of Orion KL from 325 to 360 GHz.
Shaver, P.A. 1996, Science with Large Millimeter Arrays (Springer: New York).
Shepherd, D.S., Churchwell, E., & Wilner, D.J. 1997, ApJ 482, 355.
Shen, J. & Lo, K.Y. 1995, ApJ (Letters) 445, L99.
Sofue, Y. & Irwin, J.A. 1992, PASJ 44, 353.
Thompson, A.R. et al. 1995, MMA Memo No. 142: The MDC Systems Working Group Report.
Thompson, A.R. et al. 1997, MMA Memo No. 165: System Design Considerations for the Atacama Array.
Thompson, A.R. 1997, MMA Memo No. 190: A System Design for the MMA.
Wiklind, T. & Rydbeck, G. 1986, A& A 164, L22.
Wink, J.E., Duvert, G., Guilloteau, S., Gusten, R., Walmsley, C.M., & Wilson, T.L. 1994, A& A 281, 505.
Wooten, A. 1991, GBT Memo No. 109: Long Millimeter-wave Science with the GBT.
Wooten, A. and Schwab, F.R. 1988, Science with a Millimeter Array.
Wright, M.C.H. 1997, MMA Memo No. 180: Imaging with Heterogeneous Arrays.
Yu, T. & Chernin, L.M. 1997, ApJ (Letters) 479, L63.
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