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Superconducting Integrated Receiver Superconducting Integrated Receiver Superconducting Integrated Receiver Superconducting Integrated Receiver (Development and Implementation) (Development and Implementation) Valery Koshelets, Pavel Dmitriev, Andrey Ermakov, Lyudmila Filippenko, Ad Kh d h k Ni k l Ki Ol Ki l Andrey Khudchenko, Nickolay Kinev, Oleg Kiselev, Alexander Sobolev, Mikhail Torgashin, Kotel’nikov Institute of Radio Engineering and Electronics, Moscow, Russia in collaboration with SRON Netherlands Institute for Space Research, the Netherlands

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  • Superconducting Integrated ReceiverSuperconducting Integrated ReceiverSuperconducting Integrated ReceiverSuperconducting Integrated Receiver(Development and Implementation)(Development and Implementation)

    Valery Koshelets, Pavel Dmitriev, Andrey Ermakov, Lyudmila Filippenko, A d Kh d h k Ni k l Ki Ol Ki lAndrey Khudchenko, Nickolay Kinev, Oleg Kiselev,

    Alexander Sobolev, Mikhail Torgashin, Kotel’nikov Institute of Radio Engineering and Electronics, Moscow, Russia

    in collaboration withSRON Netherlands Institute for Space Research, the Netherlands

  • Superconducting Integrated Receiver (SIR) Superconducting Integrated Receiver (SIR) with phasewith phase--locked FFOlocked FFOpp

    4 K dewarSIR chipSIS mixer

    SIR chip HEMT4-8 GHz IF

    Processor &

    Harmonic mixer

    &Digital Auto

    CorrelatorReference20 GHz

    FFO as LO20 GHz500-650 GHz

    Computer controlleddata acquisition system

    HEMTSIR

    i i it

    4 GHz

    Electronics FFO, SIS, HM control

    PLL LSU

    HEMT microcircuit

    PLL LSU400 MHz reference

    21 September, 2009 Euroflux2009, Avignon 2

  • Internal part of the SIR MicrocircuitInternal part of the SIR MicrocircuitInternal part of the SIR MicrocircuitInternal part of the SIR Microcircuit

    FFODouble-slot (dipole)twin SIS – 0.8 μm2 FFO

    400*16 μm2μ

    HM – 1.0 μm2

    Nb-AlOx-Nb, Nb-AlN-NbN; Jc = 5 - 10 kA/cm2 Nb AlOx Nb, Nb AlN NbN; Jc 5 10 kA/cm

    Optionally: SIS – Jc = 8 kA/cm2; FFO + HM = 4 kA/cm2

    21 September, 2009 Euroflux2009, Avignon 3

  • NbNb--AlOxAlOx--Nb and NbNb and Nb--AlNAlN--NbN FFO for SIRNbN FFO for SIR

    400 GHz

    Frequency Tuningq y g

    700 GHz

    JSC, VB = Vg/3

    4V.P. Koshelets, et al, Phys. Rev. B, vol. 56, pp 5572-5577, (1997)

  • NbNb--AlNAlN--NbN SIS pumped by FFO; NbN SIS pumped by FFO; FFO frequencyFFO frequency tuningtuningFFO frequency FFO frequency tuningtuning

    300 HD13-09#26 (Vg=3.7mV, Rn=21 Ohm)

    250

    300

    200

    nt (m

    kA)

    100

    150

    S C

    urre

    n

    FFO Frequency:0 GHz

    50

    100

    SIS 0 GHz

    400 GHz 500 GHz 600 GHz700 GHz

    0 1 2 3 4 5 6 70

    SIS Voltage (mV)

    700 GHz

    21 September, 2009 Euroflux2009, Avignon 5

    SIS Voltage (mV)

  • NbNb--AlNAlN--NbN SIS pumped by FFO; NbN SIS pumped by FFO; FFO t iFFO t i (f 500 GH )(f 500 GH )FFO power tuningFFO power tuning (f = 500 GHz)(f = 500 GHz)

    21 September, 2009 Euroflux2009, Avignon 6

  • FL and PL spectra of the NbFL and PL spectra of the Nb--AlNAlN--NbN FFO :NbN FFO :frequencyfrequency 660055 GHzGHz;; LW =LW = 1 7 MHz; SR = 92 %1 7 MHz; SR = 92 %frequencyfrequency 660055 GHzGHz; ; LW =LW = 1.7 MHz; SR = 92 %1.7 MHz; SR = 92 %

    25

    -20

    Phase locked

    -30

    -25 Span - 100 MHz

    Resolution Bandwidth - 1 MHzm

    ) at 605 GHz (SR = 92 %)

    Frequency locked Linewidth 1 7 MHz

    -40

    -35Bandwidth 1 MHz

    ower

    (dB Linewidth = 1.7 MHz

    50

    -45

    Out

    put P

    o

    -55

    -50

    IF O

    360 380 400 420 440-60

    Down-converted FFO Frequency (MHz)

    21 September, 2009 Euroflux2009, Avignon 7

    q y ( )

  • Phase Noise of the PL FFO

    -20

    0Spectrum analyzerResolution Banwidth RBW = 1 Hz

    -30

    Absolute FFO phase noise, (n = 20); SR = 97.7% R&S Synthesizer at 22 GHz * n2 (n = 20) Phase locked FFO, fFFO = 450 GHz (δfaut = 0.5 MHz; SR = 97.7%)) R&S Synthesizer at 22 GHz (Specification)

    -60

    -40

    Pow

    er (d

    Bm

    )

    -70

    -50

    /Hz) -100

    -80

    P

    -110

    -90

    e N

    oise

    (dB

    c/ -50 -40 -30 -20 -10 0 10 20 30 40 50Offset from carrier (Hz)

    100

    wer

    )

    -150

    -130

    Phas

    60

    80

    the

    PL F

    FO P

    ow

    10 100 1k 10k 100k 1M 10M150

    Offset from Carrier (Hz)

    20

    40

    Experimental Data; TELIS PLL JAP 102 063912 (2007)

    ctra

    l Rat

    io (%

    of

    21 September, 2009 1 100

    JAP, 102, 063912 (2007) Regulation BW = 10 MHzSp

    ec

    Free-running FFO Linewidth (MHz)

  • Development of the Integrated Spectrometer for TELIS

    Valery Koshelets, Lyudmila Filippenko, Pavel Dmitriev, Andrey Ermakov, Andrey Khudchenko, Nickolay Kinev, Oleg Kiselev,

    Alexander Sobolev Mikhail Torgashin

    g p

    Alexander Sobolev, Mikhail Torgashin, Kotel’nikov Institute of Radio Engineering and Electronics, Moscow, Russia

    Pavel Yagoubov, Gert de Lange, Hans Golstein, Leo de Jong,Pavel Yagoubov, Gert de Lange, Hans Golstein, Leo de Jong, Arno de Lange, Bart van Kuik, Ed de Vries, Johaness Dercksen,

    Ruud Hoogeveen, Avri SelegSRON Netherlands Institute for Space Research, the Netherlands

    Nopporn Suttiwong, Georg Wagner, Manfred Birk (PI)Institute for Remote Sensing Technology, DLR, Germany

    21 September, 2009 Euroflux2009, Avignon 9

  • TELIS (Terahertz Limb Sounder)TELIS (Terahertz Limb Sounder)

    TELIS Objectives:TELIS Objectives:• Measure many species for

    atmospheric science:ClO, BrO, O3, HCl, HOCl, etc;- Chemistry, Transport, Climate

    • Serve as a test platform for new sensors

    • Serve as validation tool for future satellite missions

    • Three independent frequency channels, cryogenic heterodyne receivers:

    TELIS Instruments– 500 GHz by RAL– 500-650 GHz by SRON-IREE

    ( )21 September, 2009 Euroflux2009, Avignon 10

    – 1.8 THz by DLR (PI)

  • SIR Mixer Block with ShieldsSIR Mixer Block with Shields

    21 September, 2009 Euroflux2009, Avignon 11

  • Noise Temperature of the Flight SIR Noise Temperature of the Flight SIR (DSB)(DSB)

    Water lineWater line557 GHz

    21 September, 2009 Euroflux2009, Avignon 12

  • SIR Noise Temperature SIR Noise Temperature on Intermediate Frequency and SIS Biason Intermediate Frequency and SIS Biason Intermediate Frequency and SIS Biason Intermediate Frequency and SIS Bias

    21 September, 2009 Euroflux2009, Avignon 13

  • SIR Stability:SIR Stability: Allan variance testAllan variance test

    SISPower meterIF amp

    FFO

    SISBP filter

    21 September, 2009 Euroflux2009, Avignon 14

  • SIR Spectral Resolution

    Deconvolved spectrum of the OCS emission lines at a gas pressure 2.6 mBar.

    LO f 601 GHLO frequency 601 GHz.

    Two strong lines are saturated; weaker linessaturated; weaker lines

    are not saturated isotopes.

    The lines are detected,The lines are detected, one in the LSB, the other

    one in the USB

    21 September, 2009 Euroflux2009, Avignon 15

  • Amplitude and phase APBAmplitude and phase APBof the SIR with cold opticsof the SIR with cold opticsof the SIR with cold opticsof the SIR with cold optics

    40-80.00

    -72.00

    -64.00

    20

    mm

    -56.00

    -48.00

    -40.00

    -32.00

    -24.00

    -16.00

    8 000

    40 -180.0

    -120.0-20

    0

    Verti

    cal s

    can, -8.000

    0

    20

    n, m

    m

    -60.00

    0

    60.00

    120.0

    180.0-40 -20 0 20 40-40

    -20

    0

    Verti

    cal s

    can

    Horizontal scan, mm

    Amplitude

    -40 -20 0 20 40-40

    Horizontal scan, mm

    21 September, 2009 Euroflux2009, Avignon 16Phase

  • SIR for TELIS SIR for TELIS –– remote operationremote operation

    17

  • TELISTELIS SIR M i P tSIR M i P tTELISTELIS--SIR Main ParametersSIR Main Parameters(parameters determined by digital correlator are in parentheses)

    Input frequency range, GHz 500 – 650 ГГцMinimum noise temperature in the range (DSB), K 120 КOutput IF range, GHz 4-8 (5-7) ГГцSpectral resolution, MHz < 1 (2) МГцLO f t MH < 300 МГLO frequency net, MHz < 300 МГцDissipated power at 4.2 K stage, mW < 30 мВтOperation temperature K < 4 5 КOperation temperature, K < 4.5 К

    21 September, 2009 Euroflux2009, Avignon 18

  • Esrange Space CenterSpace Center ,

    Kiruna, Sweden, 67.5oN, 21.1oE; , ;

    March 2009

    21 September, 2009 Euroflux2009, Avignon 19

  • TELIS (Terahertz Limb Sounder)( )

    TELIS-MIPAS at Esrange, Sweden; March 2009

    Balloon size: 400 000 m3; Payload weight: 1 200 kg; y g g

    21 September, 2009 Euroflux2009, Avignon 20

  • Flight trajectory (predicted)Flight trajectory (predicted)

    Flight profile (actual)Flight profile (actual)Flight profile (actual)Flight profile (actual)

    21 September, 2009 21Euroflux2009, Avignon

  • Frequencies and substances Frequencies and substances selected for the first TELIS flightselected for the first TELIS flightselected for the first TELIS flightselected for the first TELIS flight

    ## FFO Frequency GHz Substances (High priority)## FFO Frequency, GHz Substances (High priority)

    1 495.04 H2-18O

    2 496.88 HDO3 505.6 BrO (ΔТ = 0.3 К !!)( )4 507.28 ClO5 515.25 O2 /pointing /pressure5 515.25 O2 /pointing /pressure6 519.25 BrO (ΔТ = 0.3 К !!)7 607 78 O isotopes7 607.78 O3 isotopes8 619.1 HCl (HOCl, ClO)

    21 September, 2009 Euroflux2009, Avignon 22

  • Spectra measured at limbSpectra measured at limb--soundingsounding

    FFO Freq = 495 GHz

    Orbit – 30 km;

    Increment – 1.5 km,Tangent: 10.5 – 30 kmg

    45 degrees up

    O3

    Down-converted Frequency, GHz

    23

    Down-converted Frequency, GHz

  • ClO line over time (FFO = 495 GHz)ClO line over time (FFO = 495 GHz)

    Sunrise 5h08

    O3 OClO3 O3ClO

    21 September, 2009 Euroflux2009, Avignon 24

  • Back to the Earth…Back to the Earth…

    21 September, 2009 Euroflux2009, Avignon 25

  • 3030--cm POrtable Submillimeter Telescope (POST)cm POrtable Submillimeter Telescope (POST)Purple Mountain Observatory; Nanjing. Purple Mountain Observatory; Nanjing.

    Site: Delingha of Qinghai province Site: Delingha of Qinghai province (altitude ~3200 m)(altitude ~3200 m)

    Frequency - 345 GHzTr (DSB) < 100 KTr (DSB) < 100 K

    Spectral resolution < 1 MHz

    2 t GM t2-stage GM type; cooling capacity

    – 0.1 W;

    compressor – 42 kg;power consumption p p

    - 1.2 kW

    21 September, 2009 Euroflux2009, Avignon 26

  • ESPRIT ESPRIT –– Exploratory Submm Space Exploratory Submm Space RadioRadio--Interferometric TelescopeInterferometric Telescope

    • Telescope sizes ~ 3.5 meter ; off-axis• Number of elements N = 6 (15 baselines)• Projected baselines 200 - 1000 meter• Frequencies:

    Spots in the range 0.5 – 6 THz p g• Front Ends - (0.5 – 1.5 THz):

    SIS mixers, multiplier LO / SIR = FFO + SIS + HMSIR FFO + SIS + HM(1.5 – 6 THz) HEB mixers, QCL as LO

    • System temperature < 1000 KThe six elements of • IF bandwidth > 4 GHz (goal 8 GHz)The six elements of

    ESPRIT in an Ariane 5

    21 September, 2009 Euroflux2009, Avignon 27

  • “Millimetron” – Russian Space Agency ( > 2017)12 m cryogenic mirror; λ = 0 01 20 mm12 m cryogenic mirror; λ = 0,01- 20 mm.

    Ground-spaceGround space interferometer

    21 September, 2009 Euroflux2009, Avignon 28

  • Medical applicationsMedical applicationsNonNon--invasive medical diagnostics invasive medical diagnostics

    basedbased onon analysisanalysis of exhaled airof exhaled airbased based on on analysis analysis of exhaled airof exhaled air

    • human exhalation contains up to 600 volatile compounds• some of them can be used as markers of diseases

    СО Bl d di th id ti tСО Blood disease, asthma, oxidative stressNO Diseases of respiratory tract, oncologyNH Diseases of gastro-enteric tract liver kidneyNH3 Diseases of gastro-enteric tract, liver, kidneyCH4 Malabsorption of hydrocarbonsCS2 Markers of coronary arteries diseases, schizophrenia2 y pH2O2 Radiation injury, asthma

    21 September, 2009 Euroflux2009, Avignon 29

  • Gas Spectra Detection by FFTSGas Spectra Detection by FFTS

    1,0

    0,9

    0,7

    0,8

    issi

    on NH3 - 572.498 GHzP= 1 mBar

    0,6

    ,

    Tran

    sm

    P= 1 mBar 0.4 mBar 0.1 mBar0.02 mBar

    0,5 0.002 mBar

    572,3 572,4 572,5 572,60,4

    Frequrency (GHz)

    21 September, 2009 Euroflux2009, Avignon 30

    equ e cy (G )

  • Gas Spectra Detection Gas Spectra Detection -- 22

    1000

    1500

    NH3 (p= 5*10-3 mbar)

    100

    150 OSC (p= 2*10-3 mbar)

    0

    500

    nsity

    (mV)

    0

    50

    nsity

    (mV)

    -1000

    -500Inte

    n

    -100

    -50Inte

    n

    572,485 572,490 572,495 572,500 572,505 572,510-1500

    Frequency (GHz)571,110 571,115 571,120 571,125 571,130

    -150

    Frequency (GHz)

    21 September, 2009 Euroflux2009, Avignon 31

  • ConclusionConclusion

    • Concept of the Phase-locked SIR is developed and proven.p p p• Nb-AlN-NbN FFOs and SIRs have been successfully implemented. • New generation of the SIR with PL FFO for TELIS has been developed

    h i ibilit t hi ll TELIS i tshowing a possibility to achieve all TELIS requirements:Frequency range 500 – 650 GHz; Noise temperature < 150 К;IF bandwidth 4 - 8 GHz; Spectral resolution better 1 MHz; Beam Pattern - FWHM = 3 deg, with sidelobes < - 17 dB.

    • Procedure for remote SIR operation has been developed and experimentally provenexperimentally proven.

    • TELIS flight has been completed in March 2009 (Kiruna, Sweden).• Future space and ground-base missions are under consideration.• SIR Technology is mature enough for both future space missions

    and non-invasive medical diagnostic.

    21 September, 2009 Euroflux2009, Avignon 32