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MMA Memo 213: MMA Frequencies Working Gr... Band Considerations and Recommen.hp/colobus.aoc.nrao.edumemos/html-memos/mma213/memo213.
Receiver VTRw
(GHz) (GHz)
Vhigk
(GHz)
WG Band/Detector
WR-22 HFETb
WR-12 HFET
WR-8 HFET or SIS
WR-6 SIS
WR-5 SIS
n-sc SIS
n-s SIS
WR-2.2 SIS
n-s SIS
n-s SIS
Pending HFET development
Bandwidth ratio of 1.35
aBand definitions are for good sensitivity degrading increasingly beyond edges
bSome sensitivity is needed through the VLBA band. to 45 GHzc n-s means non-standard
dReceiver bands #8 and #9 are bandwidth limited by the atmosphere
Table 3: Recommended Receiver Coveragea
06/04/98 13:42:
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2
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10d
30
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89
125
163
211
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385
602
787
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79
103
144
187
243
323
442
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116
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NATIONAL RADIO ASTRONOMY OBSERVATORY949 NORHhl C4(t RR AV-NLo [ CAMP S 9l L401NG 6T IUCSON ARIZOf 8B721-0655 USAT 1t fONE (o20) 8d2 8250 FAX (510) 882 19 5 m ;lr. nuo nroo edu
'! 1 0)(0 lAllIl( MAIP
O1FL,1IANO l)1: (IIAJNAN'I'OR, C11II,1
CON1ouR INrnLVAL 10m
'OGAPHIC INOMArry IION WAS IAKEN FROml..... PHOTOGPHY (1981-1982) , INSTU IO
D Ary80 85m 36 Elemots
B OGARAICO MRITAR D CHILE , H1VN A SCALE
I A MrAy A m , 11:.
AA Array 010,000m >>36 El m
A Army Cntr N7453009.4 8628991.0
Pipche C rosing Points
Crosing A N7455582 E628019
raosaing B N7454748 E629841
Cwuaing C N7450197 E636638
GAS TAP N7455720 E627861
See crossing plan drawing & Science Preserve drawing
GA New Pipeline Location Feb. 25, 1998
Q Mm,11 88.L GM fl dmg
4I I a6a-
Chajnantor, 50m Contours
620 625 630 635
UTM X [km]
7465
7460
7455
7450
O*tv QptyDIibaiQPa
QtO0025Q)5 0075 0.1 0:125 .1504
225-GHz Zenith Opacity (Nepers)
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MMA SENSITIVITY GOALS
Continuum - In 60 seconds of integration time the RMS flux densityacieved is:
Frequency AS(0 Hz) (miy)
35 0.067
90 0.065
140 0.056
230 0.080
345 0.14
650 0.48
Spao~i. -kb 6 secs ofinI ia im the RMS flux density
aiiieed- l h dsa w;b oI I stL Id 25 km s - respectively is:
Freueecy L (1 mr -s-") AS (25 m s-')
35 Is 3.5
90 10 2.1
14011 2.2
230 13 2.6
345 18 3.5
650 43 8.6
TABLE 4.1 OVERVIEW AND COMPARISON OF MMAINSTRUMENTATION GOALS
ANTMAS
RS& Slce Accuacy
Fast Sw~icingTotal Power bserving
RECEIVERS
28-45 GHz HFET
67-965 GHz EFET
91-119', G SIS or H ET
125-463 GHz SIS
1:63-I21 GHz SIS
211-275 GHz SIS
275-370 H1z SIS.386-506 I00Ci S1S
60Z-720 iIc G 5S1
787-9 G SIS
Ss Iaanced Miers
SIS Image Separatging
S IIn wiidrIF
Io
.adiig.
< 25 microns
0.8
Cycle < 1Os
Yes
Yes
Yes
Yes
Yes
Yes
YesYes
Yes
Yes
Pl ed
Yes
Yes
Yes
Yes
2x 8 GHz
30-80 microns
> 3"
No Capability
No Capability
Special Purpose only
No Capability
Yes
NRO only
No capability
Yes
No capability
No capability
No capability
No capability
No
No
No
No
2 x. I GHz
MMA: SCHEDULE AND COST
1. Design and emeopmet Phase FY98-00
- Assess p~g tit pe haidwau for peafoumance;
-estabish anm rdiitale" os ~ais for MMA construction;
- choose a site
- confirm a 25 percent iimvwofeet of external (to the NSF)partnes in the MMA for consructionand operations.
2. Cnstctionand Cost
- Costruction isplanned for the six year 2001 -2006.
Te A st esii ais $2~OtM (1998 dollars).
- A~al oa ti~ costis es to be $8.5 (1998d sOi s.
MMA DESIGN AND DEVELOPMENT1998 - 2001
GOALS* Paper design of all major MMA components.
* Prototypes of critical or high-risk instruments.
* Decision of design options.
ANTENNA: Prototype designed and built under contract, erected on VLA site.
RECEIVERS: Prototype SIS mixers at two bands.
* Image separating.
* Balanced.
* Integrated with IF amplifier.
* Scaleable to all MMA bands.
LOCAL OSCILLATOR: Working prototypes of two types and decision.
* Planar vacator multiplier chain.
* Photonic
CENTRAL LO, IF, AND FIBER OPTICS* Paper design of major components.
* Breadboards of representative modules
CORRELATOR
* Single baseline GBT-clone.
* Definition of MMA design.
COMPUTING
* Support of antenna/interferometer testing.* Clear set of MMA specs from community.
MMA TIMELINE
1998 - 2001
2001 - 2003
2004 - 2007
Design and Development* Complete project WBS cost and schedule.* Paper designs and prototypes.
Instrument Evaluation on Test InterferometerSite Engineering and Civil WorksOSF Buildings on site and in SPdA.Initiate Production Fabrication
Delivery and Outfitting of Nine (9) Antennas a YearInterim Operations
Commissioning, Retrofits, and Operationzoos - 201o
MILLIMETER ARRAYNational Radio Astronomy Observatory
&A teity of the National Seleae FeunLdatin operated undereep rati dreeat by Asseetated Unie atie. Inc.
ITEM SPECIFICATION NOTES
APERATURE SIZE 10 METER MINIMAL BLOCKAGE
NUMBER OF ANTENNAS 36 TRANSPORTABLE
SITE CERRO CHAJNANTOR, CHILE 5000 METER ELEVATION
FREQUENCY RANGE 30 GHZ TO 950 GHz
SURFACE ACCURACY 25 MICRONS RMS
POINTING ACCURACY 0.8 ARCSEC 1/30 PRIMARY BEAM @ 300 GHZ
PHASE STABLITY 10 MICRONS RMS MEDIAN WIND CONDITIONS
CLOSE PACKING <I.25D MINIMAL BASELINES
DYNAMIC PERFORMANCE 1.5°
IN I SEC @ 3" POINTING FAST SWITCHING FOR CALIBRATION
SLEW VELOCITY 3"/SECOND AZIMUTH & ELEVATION
ACCELERATION 12°/SECOND SQUARED AZIMUTH & ELEVATION
RESONANT FREQUENCY >7 HZ LOWEST MODE
SUBREFLECTOR 3 BEAMWIDTHS AT 86 GHZ NUTATION
OPTICS CASSEGRAIN MINIMAL REFLECTIONS
RECEIVER CABIN SIZE 3 M X 3M X 2.6 M RECTANGULAR BOX
CAIN DooR IMx 2 M
ELEVATION RANGE 12700 FROM NORTH
AZIMUTH RANGE 0. TO 95°
PANELS 120 MACHINED ALUMINUM ~1 SQUARE METER IN SIZE
MAXIMUM WIND SPEED 65 M/SEC SURVIVAL
MEDIAN WIND 9 M/SEC EVALUATION OF SPEC.
ENVIRONMENT FULL EXPOSURE VOLCANIC SOIL & GRAVEL
NRAO 10 METER DESIGNJUNE 2, 1998
LUGTEN, KINGSLEY, CHENG & FLEMMING
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6/5/98 8:47 Pi ofI I
SINGLE DEWAR RECEIVER LAYOUTMMA Receiver
MARCH 21,Group
1997
-DEWAR TOP
A 30-48 GHzB 67-95 GHzC 94-133 GHz0 132-183 GHzE 182-236 CHzF 235-307 GHzG 305-400 GHzH 397-517 GHz1 602-720 GHzJ 787-950 GHz
-A BAND LENS SOCKET
-RADIATION SHEILD
-DEWAR
S0 1 2 3 4 5, . .... _________ I_ ___ _, ,__SCAL, I
SCAL
DEWAR RECEIVER LAYOUTSMMA Receiver Group
APRIL 15, 1997
-DEWAR TOP
A 30-48 GHzB 67-95 CHzC 94-133 GHzD 132-183 GHzE 182-236 GHzF 235-307 GHzC 305-400 GHzH 397-517 GHzI 602-720 GHzJ 787-950 GHz
PAYNE-K ERR-KINGSLEY
7.0 7.25
LUGTEN-WELCH
0 . 2 3 4 5
SCALEu
--
L o AL O eS LL RTO* S
TWO SYSTEMS BEING CONSIDERED
CONVENTIONAL
Gunn oscillator or YIG oscillator followed bymultipliers
Advantages
* Proven technology
* Will work
Disadvantages
* Expensive
* Very few commercial suppliers
* Several highly specialized devices perband
BASIS OF METHOD
I'
DETECTOR
LASER 2 12MICROWAVESIGNAL OUT
(f1 - f2)
REQU UIREMENTS
LASERS
1. A = 1.5p (200 TH:z, so we can usecommercially developed fiber opticcomponents.
2. High spectral purity.
3. Easily incorporated into a phase lock systemlocked to an external microwave reference.
4. For ease of operation, the lasers should beset-able open loop to a few MHZ.
5. Single mode operation.
6. Linear polarization.
Schematic of Lonj, Wavelength Velocity-Matched Distributed Photodetector (VMDP)
. .. .=" ' , ........ ; I.r: ,ic~ " ' :'";~i~ i1 ......... .... .... . ....III. ..II I. ..
* Photocurrents add in-phase through a 50coplanar strips microwave transmission line thatis velocity-matched to the optical waveguide
CoplanarStrips
OpticalWaveguide
InAIAs Upper Cladding II
InAIGaAs Upper Cladding
InAlGaAs Waveguide Core
InAlGaAs Lower Cladding InP Substrate
Active MSMPhotodiodes
layer structure:
InAlAs Schottky Barrier layerInGaAs/InAIAs Graded SuperlInGaAs Absorption layer
Integrated Photonics Laboratory JIl
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With electro-optic devices, phasemodulation is achieved by aligning the
upM.Iy dacive axis. New hocus makesproper alignment easy; simply pass thebeam through the mechanical apertures.
Researchers at JILA, University ofColorado and National Institute of
Standards and Technology, and NewFocus have recently used a prototypeModel 4851 that resonated at 10.5 GHzto generate a spectrum of sidebandsover 3-THz wide around a stabilized633-nm HeNe laser source.* (That'sover 250 sidebands at 10.5-GHz spac-ings!) Typically, phase modulation onlyproduces a few sidebands. (See page 42for a discussion of sideband generation.)However, by combining the efficiencyof the Model 4851 with an optical res-onator, the researchers were able to pro-duce the spectrum shown in the graph.
Called optical comb generation, thistechnique produces a series of equallyspaced spectral lines that extends overa wide frequency range around a cwoptical carrier. One important applica-tion of optical comb generators is forhigh-resolution spectroscopy of variousmolecular and atomic transitions. Thesestudies are usually performed with alaser locked to a well-known frequencyreference, which limits one to studyingtransitions close in frequency to thelaser frequency. In contrast, because
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The graph shows the output spectrum ofthe comb generator measured using aFabry-Perot cavity with a 2-THz free-spectral range.
9 8 0 - 8 0 8 8 f a x :- ( 4 0 8 ) 9 8 0 - 8 8 8 3
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optical comb generation enables widefrequency intervals to be coherentlylinked, a frequency-stabilized laser withan optical comb generator can be usedto study transitions that are far from thelaser's center frequency. For instance, astabilized HeNe laser and an opticalcomb generator can be used to studyseveral molecular iodine absorptionlines around 633 nm as well as a neontransition that occurs at 633.6 nm.
*J.Ye, L-S. Ma,T. Day, and J. L Hall,"Highly-selective terahertz optical fre-quency comb generator," Optics Letters,22, No.5, (1997).
I
TERAHERTZ OPTICAL COMB GENERATOR
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Feasability of HEMT-Amplifiers
1. Frontend Amplifiers
Amplifiers for cryogenic operation with InP-HEMTs have been developed atthe MPIfR for the frequency-bands:
12 - 18 GHz18 - 27 GHz26.5 - 40 GHz33 - 50 GHz
The noise contribution of these amplifiers is < 0.5 RF-Frequency/GHz
The frequency band 50 - 75 GHz can be covered by hybrid amplifiers withexisting 0.1 x 40 micron TRW-InP-HEMT devices. Amplifiers for 75 - 100GHz are presently under development.
The MPIfR is taking part in the JPL/NASA Cryogenic HEMT OptimizationProgram (CHOP) and evaluates single HEMT devices for the development ofhybrid amplifiers and cryogenically coolable MMIC's produced by TRW.The institute has a proberstation for 300 K and will soon also have acryogenic proberstation for the evaluation of HEMTs.
2. IF-Amplifiers
IF-amplifiers covering 4 - 8 GHz or 8 - 16 GHz should be feasable asbalanced hybrid amplifiers, thus reducing the influence of the mismatchbetween SIS-mixer output and amplifier input, provided that the procurementof InP-HEMTs with a 0.1 x 300 micron gate geometry is possible. Adevelopment of a balanced IF-amplifier with PHEMTs is currently under way.
With respect to the numerous channels a balanced MMIC solution shouldalso be taken into consideration.
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30-50GHz AmplifierHot/Cold-Measurement, Systemtemperature including input loss and IF
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29,8 31,4 33f/GHz
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CENTRO ASTRONOMICO DE YEBESOBSERVATORIO ASTRONOMICO NACIONAL
(SPAIN)
8-12 GHz cryogenic amplifier for FIRST with InP (June 98)
Test with InP HEMT only in 1 stage, not optimized for flat gain.
transistor type (1" stage): InP PHEMT, 0.1x160 pmpower dissipation (1" stage): 5 mW (optimum bias)Average Noise Temperature: 6.5 K (Tamb=15 K)
Gain: ~23 dB
YXF 003 (InP 160m 1st stage)30
20
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60
50
40
30 Y
20
10
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0 I
6 8 10 12
Freq. (GHz)
CENTRO ASTRONOMICO DE YEBESCAY OBSERVATORIO ASTRONOMICO NACIONAL
(SPAIN)
8-12 GHz demonstration cryogenic amplifier for FIRST (Feb. 98)
Isaac L6pez Fernandez
Juan Daniel Gallego Puyol
transistor type: GaAs PHEMT, 0.25x200 pmtotal power dissipation: 10 mW
Average Noise Temperature: 14 K (Tamb=15 K)Gain: -20 dB
YXF 00130 60
- 50\ Gain (model)
20 --o- Gain (measured) /0 40
20 / ao 0
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0 1 0I6 8 10 12 14
Freq. (GHz)
CENTRO ASTRONOMICO DE YEBESOBSERVATORIO ASTRONOMICO NACIONAL
(SPAIN)
Noise Temperature of Wideband IF Cryogenic Amplifiers (estimated)
40
30
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Freq (GHz)
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LSA Local Oscillators
* LOs are a technically demanding and may well be an important instrurdriver in a similar way to FIRST.
* Definition of frequency bands required.
* Thought must be given to the best method of signal and LO coupling.
* Simple, proven and reliable systems should be used whenever possibleorder to reduce manufacturing cost and increase chances of success.
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Rutherford Appleton Laboratory LSA-RWG Meeting Leiden 8 June 98 1
MMT Varactor Frequency Multipliers
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ESA Workshop on Millimeter Wave Technology and Applications.May 27-29, 1998. Millilab, Espoo, Finland
RECEIVERS FOR GROUND BASED MM WAVE RADIO TELESCOPES
A. Karpov
Institut de Radioastronomie Millimetrique, 300, rue de la Piscine, Domaine Universitaire de Grenoble.F-38406 St. Martin d'Heres, France
ABSTRACT
We present a study of requirements on the sensitivity of mm and sub millimeter wave receivers for application inradio astronomy. The study is based on the experience of the operation of the SIS receivers at the radiotelescopes of IRAM and considers also the conditions of operation at the future radioastronomical instrumentssuch as LSA, MMA and LMSA.Using a radio telescope and atmospheric model we consider the effect of the receiver sensitivity on the radiotelescope operation in terms of observing time. The observing time at a radio telescope depends on the systemnoise temperature as strongly as on collecting area, which defines nearly all the cost of modern mm and sub mminstruments. As a compromise between the receiver development effort and the system performance we introducea criterion of an "optimum" receiver noise. A strict requirement on the receiver operation is obtained. For anefficient use of the existing and the future radio telescopes, a 10 - 20 K SSB receiver noise in the mm band and20-40 K SSB at sub millimeter wavelength are necessary.Finally the status of development of SIS receiver for mm and sum mm radio astronomy is presented.
Keywords: low noise receivers, radio telescope, millimeter wave, SIS receiver.
1. INTRODUCTION
Radio astronomy is a domain where the most sensitive millimeter wave receivers are required [1,2]. Theperformance of the receivers in millimeter wave radio astronomy is based on development of low noise, broadband and stable SIS mixers [1,2]. Having as a basic limitation only the quantum noise limit of hu/k for the SSBnoise temperature they may remain as the basis for the construction of new observing facilities. Theinconveniences such as the cooling to the liquid helium temperature and sometimes the mechanical tuning forSSB operation remain less important compared to the strict requirement on the receiver sensitivity for an efficientuse of the radio telescopes, impossible with other types of receiver.
A further development of millimeter wave radio astronomy instrumentation is related to the construction of thebig interferometers such as the Large Southern Array (LSA)[3], Millimeter Array (MMA)[3], or LargeMillimeter and Submillimeter Array (LMSA)[4] planned to integrate 50-60 antennas of 10-15 m in diameter atthe high altitude plateau in Chile, at about 5 km of elevation. The new instruments will have a collecting areamore than 10-20 time larger than in existing instruments such as the IRAM radio interferometer [6].
In preparing such new instruments for mm and submillimeter wave radio astronomy an important work on thereceiver development has to be undertake. One can put forward once more a question about an optimum designof the receivers for these instruments and about their role in the system performance for the existing context ofreceiver and telescope technology and for the future.
As a starting point for a discussion one can use an example the case of existing radio interferometers, such as theIRAM five 15 meter antenna interferometer in the French Alps at 2500 m altitude. The IRAM radiointerferometer at the Plateau de Bure (PdB) is an instrument with the biggest collecting area developed for theradio astronomy observations around 1 mm wavelength [6]. We are using the PdB radio telescopes data as anexample of a modern instrument for an estimation of the role of the receivers in the existent context. First we givea presentation of the requirements on the receivers for the IRAM installations based at our IRAM internal report[7]. Then we study the requirements on the receiver sensitivity for the future instruments and present the status ofthe SIS receiver development in IRAM.
ESA Workshop on Millimeter Wave Technology and Applicalnur.
May 27-29. 1998, Millilab, Espoo, Finland
2. OPTIMUM NOISE RECEIVERS FOR IRAM RADIO TELESCOPES
The reduction of the receiver noise always reduces the integration time required for an observation. Nevertheless
some reasonable minimum of the receiver noise may be evaluated. The requirement on the sensitivity of a
receiver may be formulated in terms of the optimization of the radio telescope system performance. including the
receiver, the telescope and the atmosphere. As an optimization criterion we can use the relative speed-up of
observations at a telescope versus receiver temperature. As a reference value, not affected by the receiver
operation, we take the observation time necessary for detection of a certain signal with the same telescope in a
hypothetical situation of zero receiver noise. The relative variation of integration time is estimated from the
relative variation of the system noise temperature:
t/t, ={ T *,sT (TRec) T *s (Tec = 0) } (1)
An acceptable increase in observation time has to serve as a compromise between the receiver developmenteffort and the system performance. One can use a 50 % increase in observation time. not negligible indeed, as acriterion for the estimation of the optimum receiver noise for radio telescopes.
The system noise temperature T*Sy s is calculated according to [8]:
S 1+ GI / Gs [F, .T +(1-F, ) Tab + TRe]SF,I exp(-A t0)
(2)
where T*svs is the radio telescope system noise temperature at the "star scale" in a reference plane out of the
atmosphere; Tsky, Tamb and Trec are respectively the sky antenna temperature, the ambient temperature and the
receiver noise temperature: Gs and Gi are respectively the signal and image band conversion gain, Feff is the
forward efficiency; z 0 is the sky zenith opacity.
The sky antenna temperature Tsk is calculated as:Tsk, = Ta,, [1- exp(-A')]
where the airmass A is: A and a is the telescope elevation angle. Comparing (1) and (2) one cansin(a)
mention that the speed-up of observation (1) does not depend on the sideband ratio Gs/Gi , but only on the value
of Trec. So, the requirements on the value of receiver noise listed below concern equally observations with a
Double Sideband receiver (Trec DSB) or with Single Sideband receivers (Trec SSB). As the major part of most
observations is in SSB mode, we will discuss especially the requirements on Trec SSB.
We selected the different typical frequencies as 90, 230, and 345 GHz and proceed our calculations for severaldifferent atmospheric conditions. We studied "good" summer weather (7 mm Precipitable Water Vapor (PWV)),
the "average" winter/good summer conditions (4 mm PWV) and "good" winter weather (2 mm the PWV). At 345
GHz we consider also an "excellent" winter weather (0.5 mm PWV). This estimation concerns both the IRAM
Plateau de Bure Interferometer and the 30 m IRAM Pico Veleta (PV) telescope for the following reasons. The
forward efficiencies of the two types of antennas are the same within 1%, at least in the 3 mm (90%) and 1.3 mm
bands (86 %). The estimation at 345 GHz concerns first the 30 m radio telescope with a 75% forward efficiency.
The typical values of the atmospheric opacity are also similar at the two sites [9].
An example for a frequency of 90 GHz is shown in the figure 1. Here the relative fraction of the system noise dueto a non zero receiver noise (T*sys(Trec)-T*sys(Trec=O)}/T*sys(Trec) is plotted against Trec at the left. First we
can say that the receiver noise gives a significant part of the system noise and the receiver noise may easilydominate in the system operation.
We obtain a more clear presentation of the receiver noise role by estimating the time required for the detection of
an astronomical signal, determining the number of the astronomical project one can schedule at the telescope. In
the right part of the figure 1 is plotted the relative increase of the radio telescope observation time (I) versus the
receiver noise. One can see that in typical weather the observation time of a modern radio telescope strongly
depends on the receiver noise. With a moderate 50 K receiver noise the observation time has to be 4 time longer,
than the minimum at a zero receiver noise. This corresponds to the loss of a half of the radio telescope collecting
area, or. what is nearly the same, the loss of the half of the funding for a radio telescope. Only by approaching an
"optimum" TRec Opr=1 0
K receiver noise one can achieve an observation time only 50% longer than theminimum.
ESA Workshop on Millimeter Wave Technology and Applications.May 27-29, 1998, Millilab. Espoo, Finland
This "optimum " receiver noise of 10 K SSB required at 90 GHz for the existing radio telescopes is ftar better thebest published results of 60 K SSB of an SIS receiver at NRAO Keat Peak radio telescope [10]. In our recent SISreceiver prepared for installation at the PdB interferometer the SSB receiver noise ranges between 30 K and 48 Kin the 80-120 GHz band (figure 6).
The estimation of observation speed-up versus receiver noise is plotted in the figure 2 for frequencies of230 GHz and 345 GHz. In this typical condition even with a bigger atmospheric opacity the time required for thedetection of an astronomical signal strongly depends on the receiver noise. The 150% threshold compared to theminimum observation time can only reached with a 20 K SSB receiver noise at 230 GHz and 30 K SSB at 345GHz. For the moment the best SSB receiver noise at these frequencies is about 50 K (figure 6).
0.8
0.6
0.4
0.2
00
Receiver Noise Temperature [K]
20 40 60 80 100
Receiver Noise Temperature (K]
Figure 1. The contribution of a receiver to a modern mm wave radio telescope system noise temperature (left)and the influence of the receiver noise at the time of observation (right) at 90 GHz. We are using an example ofthe IRAM 30 m radio telescope at Pico Veleta or IRAM 15 m radio telescopes of the Plateau de Bureinterferometer. The antenna is at 45
° elevation, forward efficiency is 92% and the altitude is 2500-2800 m. A
solid line represents an average summer weather (7 mm PWV), a dotted line - a good summer/average winterweather with 4 mm PWV and a dashed line - a good winter weather with 2 mm PWV. In a typical weather themm wave receiver noise may easily dominate the operation of a modern radio telescope and to increase stronglythe observation time. With a 10 K receiver noise a time required for an observation is still longer than theminimum by 50%.
/
- 7 -
0 40 80 120 160 200 0 40 80 120 160 200
230 GHz Receiver Noise Temperature ([K 350 GHz Receiver Noise Temperature (IK
Figure 2. Estimation of a relative increase of the radio telescope observation time at 230 GHz (left) and 350 GHz(right). The Forward efficiency at 230 GHz is 86% and 75% at 350 GHz. The conditions are the same as in thefigure. For the 350 GHz data we add an estimation in "excellent" win:er weather with 0.5 mm PWV (dotted-dashed line). In a good weather, when the observations are the most rapid, the observation time strongly dependson the receiver sensitivity, until we reach a 20 K receiver noise at 230 GHz and 30 K at 350 GHz.
ESA Workshop on Millimeter Wave Technology and Applications.May 27-29, 1998, Millilab. Espoo, Finland
3. RECEIVER FOR THE LSA/MMA SITE OBSERVING CONDITIONS
At about 5000 m altitude at a new site studied for the LSA/MMA/LSMA projects the weather is much better thanat the existing radio telescope locations. Here the PWV below 0.5 mm is observed about 25-30 % tof the time
("good" weather) and for about 75% of the time the PWV is below 1.5 mm ("average" weather) [4,11]. Forcomparison at the IRAtM radio telescopes only in "good" winter time weather the is PWV below 1.5 mm forabout 25% of the time and below 5 mm 75% of the time in "average" weather. In these new conditions therequirements on the receiver sensitivity are even more severe and demand further progress in sensitivity.
The transmission through the atmosphere with 0.5 mm, 1.5 mm and 5 mm PWV is plotted with the typical valuesof the forward efficiency FEffexisting at IRAM radio telescopes in the figure 3. The loss in the radio telescope(FEf) is a minor contribution in the total loss at the IRAM radio telescopes in "average" weather with 5 mmPWV, and gives just half of the total loss in "good" weather. At the new site this level of the loss will dominateloss in the atmosphere and can not to be accepted.
One can expect that with progress in technology FEff will be increased up to the maximum existing now at 100GHz, of about 92%. Below we will use this value for the estimations for a 60 GHz - 550 GHz frequency range.
1
0.9
0.8
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- 0.2
0.1
0
50 150 250 350 450 550
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Figure 3. The atmospheric transmission with 0.5 mm. 1.5 mm. and 5 mm PWV (from upper to lower curve) andthe forward efficiency at the IRAM 30 m radio telescope. The PWV level is below 1.5 mm at the 30 m telescopesite about 25% of winter time, and about 75% of the winter time below 5 mm PWV. At the LSA site the PWV isbelow 0.5 mm during the 25% of observing time and below 1.5 mm PWV during 75 % of the time. At theexisting radio telescope the loss related to the forward efficiency is not dominating the atmospheric loss, but atthe LSA site the forward efficiency may be the main limiting factor of the system sensitivity.
The "optimum" receiver noise TRec Opt required for the atmospheric conditions of figure 3 is summarized in thefigure 4. Here we are using for TRec Opt the relation (3) obtained from (1) and (2) for a relative increase ofobservation time r/t0 = 1.5.
TRecope = (1j'. -1)(FEf T , +(1- Ff )Tm,,h) '3)
The "optimum" receiver noise depends on the forward efficiency, and through the sky antenna temperature on thezenith opacity. For a fixed FEff the minimum TRec Opt required with a zero zenith opacity is:
Min(TRecop,) = (S - 1)(1- FEf )T,,n' (4)
about 6 K with FEff=92%. Under the same conditions the maximum of the TRec Opt corresponds to animportant atmospheric opacity, and is about 60 K. independent of the frequency:
Max(T cop,,,) = (1 - 1)(Tmb - F (T\mb T- (t))
. --- ,Forward Efficiency
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ESA Workshop on Millimeter Wave Technology and Applications.May 27-29, 1998, Millilab, Espoo, Finland
ESA Workshop on Millimeter Wave Technology and Applicati,May 27-29, 1998. Millilab. Espoo, Finland
Applying the criteria of an "optimum" receiver noise to the typical conditions of the existing mm wave radiotelescopes, one need the receivers with the 10-20K SSB noise in the mm band. and the 30-40 K in the submmband. For the futures radio telescopes the requirements are more strict, and become 10 K SSB in the mm bandand 15-40 K at the submm wavelength.
The sensitivity of the existing SIS receivers developed in IRAM for radio astronomy is between 30 K SSB and50 K SSB in the 100 GHz - 350 GHz band and must be further improved for application in the future projectsdiscussed above.
I I
j1. _ i II ? I
50
_ 40
S20
10
050 100 150 200 250 300 350 400 450 500 550
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° and the forward efficiency is supposed to be 92% at all the
frequencies. The straight line corresponds to the quantum limit of the receiver SSB noise temperature hv/k. If the
receiver sensitivity required for the average winter weather of IRAM radio telescope (gray line) ranges between13 K SSB at 100 GHz and 50 K SSB at 345 GHz, at the new LSA/MMAILSAM site it become 10 K - 30 K SSB.
50 125 200 275 350
Frequency [GHz]
425 500
Figure 5. The minimum system noise temperature of a radio telescope at the LSA site with the "optimum"receiver noise temperature. The conditions are the same, as in the figure 4.
4. THE STATUS OF THE MM WAVE SIS RECEIVER DEVELOPMENT IN IRAM
The status of the mm wave SIS mixer heterodyne receiver development in IRAM is presented in Figure 6. Theminimum SSB receiver noise achieved around 345 GHz is 48 K, about 2.8 hs/k, around 230 GHz the minimumDSB receiver noise is about 50 K and 30 K at 90 GHz. The motivation of this development is the optimization ofsensitivity of existing radio telescopes and the preparation of a new generation receiver at the level ofrequirements for the future instruments like LSA and MMA, or LSMA.
5. CONCLUSION
The requirements for the sensitivity of mm wave receivers for ground based radio telescopes have beendiscussed. Using a radio telescope and atmospheric model we consider the effect of the receiver sensitivity on theradio telescope operation in terms of the observing time. The observing time at a radio telescope depends on thesystem noise temperature as strongly as on collecting area, which defines nearly all the cost of modern mm andsub mm instruments. As a compromise between the receiver development effort and the system performance weintroduce a criterion of an "optimum" receiver noise allowing to obtain the detection time 50% longer than withzero receiver noise.
90
60
30
50 150
Frequency [GHz]
Figure 6. The measured receiver noise temperature of the SSB and DSB SIS receivers developed in IRAM [12-15]. The SSB receiver noise is given by the round points 0 and the DSB noise - with the square points G.
6. REFERENCES
I. J. E. Carlstrom and J. Zmuidzinas, "Millimeter and submillimeter techniques", in "Reviews of Radio Science 1993-1995" ed. W. R. Stone, Oxford, The Oxford University Press, 1996.
2. R. Blundell and C.-Y. Tong, "Submillimeter receivers for radio astronomy", Proceedings of IEEE, Vol. 80. pp. 1702-1720. 1992.
3. D. Downes. "Large southeren array", An IRAM-ESO-OSO-NFRA Study project, 1995.4. J. E. Carlstrom, "The Millimeter Array", Proceedings of the Seventh International Symposium on Space Terahertz
Technology, March 12-14. 1996, Charlottesville, VA, pp. 17-28. 1996.5. M. Ishiguro, "LMSA", Proceedings of the 19th International Conference on Infrared and Millimeter Waves, ed. K.
Sakai and T. Yoneyama, JSAP, p. 246, 1994.6. S. Guilloteau et al, "The IRAM interferometer on Plateau de Bure", Astronomy and Astrophysics, No 262, pp. 624-
633, 1992.7. A. Karpov, J. Blondel, "SIS mixers for the new receivers of PdB interferometer", IRAM internal report 232/95.8. M. Guelin, C. Kramer, W. Wild. "Cookbook Formulae for Estimating Observing Times at the 30 m Telescope".
IRAM Newsletter, N 19, pp. 17-23., January 20, 1995.9. G. Duvert, "Le temps A Bure", IRAM annual report 1990, p. 32, 1990.10. J. M. Pain. J. W. Lamb, J. G. Cochran, and N. Bailey, "A new generation of SIS receivers for millimeter wave
radioastronomy", Proceedings IEEE, Vol 82, N 5. pp. 811-823, May 1994.11. K. Kono et at, "Preliminary results of Site testing in Northen Chile with a portable 220 GHz radiometer, NRO
Technical report N 42. 1995.12. A. Karpov, J. Blondel, M. Voss, K. H. Gundlach. "A single sideband submillimeter SIS receiver with a 3hv/k noise",
Proceedings of 5th International Workshop on Terahertz Electronics. September 18-19. 1997, Grenoble, France.13. A. Karpov. J. Blondel, K. H. Gundlach, D. Billion-Pierron, "Low noise SIS mixer for 230 GHz receivers of Plateau
de Bure Intertferometer", International Journal of Infrared and Millimeter Waves, N 2. pp. 301-318, February 1997.14. A. Karpov, J. Blondel, P. Pasturel, K. H. Gundlach, "A 125-180 GHz fixed-tuned SIS Mixer for Radio astronomy",
IEEE Transactions on Applied Superconductivity, Vol. 7, N 2, pp. 1073-1076. 1997.15. A. Karpov, J. Blondel, M. Voss. K. H. Gundlach. "Four photons sensitivity heterodyne detection of submillimeter
radiation with superconducting tunnel junctions", IEEE Transactions on Applied Superconductivity, Vol. 5, No. 2.pp. 3304-3307, 1995.
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Proposed NOVA LSAIMMA Receiver Development
-ASSUMPTIONS AND CONSIDERATIONS
- PHASES IN THE LSA/MMA PROGRAMME
- RECEIVER PRODUCT TREE
- NOVA DEVELOPMENT ACTIVITIES
- ACTIVITIES
- PROGRAMMATICS
ASSUMPTIONS AND CONSIDERATIONSII_
- LSA/MMA ORGANISATION T.B.D.
- RECEIVER DEVELOPMENT AND CONSTRUCTION CARRIED
OUT IN USA AND EU
- EU RECEIVER EFFORT IS A COORDINATED DEVELOPMENT
AND CONSTRUCTION: REQUIRES ONE INTERFACE TO
LSA/MMA; NOVA EFFORT PART OF IT
- US MMA RECEIVER DEVELOPMENT ALREADY STARTED;
NOVA INITIATIVE ALLOWS EU TO START AS WELL
- DETAILED RECEIVER WORKPLAN AND ORGANISATIONAL
SETTING TO BE ARRANGED IN SECOND HALF OF 1998.
- INVOLVED PARTIES: RECEIVER WORKING GROUPS AND
LSA/MMA PROJECT
PHASES IN THE NOVA LSA/MMA RECEIVER PROGRAMME
- NOVA HAS FUNDING FOR 10 YEAR RECEIVER DEVELOPMENT
FOR THE LSA/MMA
- COVERING FIRST DAY RECEIVERS AND SECOND
GENERATION
- COVERING RESEARCH AND TECHNOLOGY DEVELOPMENT
- FUNDING STOPS AFTER DEMO MODELS, WHERE "MASS"
PRODUCTION STARTS
NL MAY BE A CANDIDATE "PI" INSTITUTE
NOVA LSA/MMA RECEIVER PROGRAMMATICS
- EMBEDDED IN FIRST-HIFI DEVELOPMENT
- MIXER DEVELOPMENT AT SRON/RUG
- JUNCTION DEVELOPMENT AT RUG/APPL.PHYS.DEPT
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- JUNCTION MATERIALS FOR QLP ATHIGH FREQUENCIES
- PRODUCTION YIELD AND PERFORMANCE BANDWIDTH
- DESIGN AND DEVELOPMENT PROTOTYPE CRYOSTAT
- INPUT OPTICS
- LO COUPLING AND LOCATION LO
- MECHANICAL /THERMAL LAY-OUT
- IF-AMP MODULE
- BIAS MODULE (ASICS DEVELOPMENT)(LOCATION OUTSIDE)
- RELIABILITY/SERVICING
- PREPARATION FOR INDUSTRIAL PROCUREMENT
OF MIXER AND OTHER RECEIVER COMPONENTS
PILOT PRODUCTION RUNS
SURVEY AND IDENTIFY INDUSTRIAL PARTNERS (ADDITIONAL FUNDING
SOURCES?)
- DEVELOPMENT OF INTEGRATION AND TEST PLAN
- POSSIBLE SCENARIOS
- BUDGET ESTIMATES
SYNERGETICS LSA/MMA AND HIFI PROJECTS
LSA/MMA FIRST-lIFI
FREQUENCY RANGE 70- 950 GHz 480-2700 GHz
IF CENTER T.B.D. 4 OR 10 GHz
IF BANDWIDTH 4-8 GHz 4 GHz
MIXER TYPE WAVEGUIDE WAVEGUIDE/QO
CORRUGATED HORN CORRUGATED HORN
SIDE BAND SSB DSB
TUNERLESS YES YES
JUNCTION TYPE SIS Nb/A102/Nb SIS Nb/A102/Nb
TUNING STRUCTURE NbTiN NbTiN
QUAL. LEVEL HIGH SPACE
MODULAR DESIGN Y Y
COMMON CHARACTERISTICS:
- NEED FOR MODULARITY: ASICS DEVELOPMENT
- COUPLING OF MANY LO'S INTO CRYOSTAT:WINDOW DEVELOPMENT
- COMPUTERIZED TESTING AND CONTROL: EASY RESET OF RECEIVERS
EFFICIENT AND RELIABLE OPERATION
- LARGE MTBF REQUIREMENT
NOVA LSA/MMA Receiver Project
Management Structure
Personnel: Project manager (WO), 2 WO's, 2 HBO (halftime), project scientist.Ut U !
Cost to NOVA: 4.3 million guilders
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