fsue “lavochkin association” lebedev physical institute astro space center millimetron mision...
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FSUE “Lavochkin Association”Lebedev Physical InstituteAstro Space Center
Millimetron mision sensitivities and Millimetron mision sensitivities and instrumentation conceptinstrumentation concept
A.M. Baryshev, W. Wild, G. Goltsman, N.S. KardashevA.M. Baryshev, W. Wild, G. Goltsman, N.S. Kardashev
Netherlands Institute for Space Research, NetherlandsNetherlands Institute for Space Research, NetherlandsAstro Space Center, Lebedev Physical Institute, RussiaAstro Space Center, Lebedev Physical Institute, Russia
ISSTT 2008, Groningen 2
OutlineOutline
• Main concept of “Millimetron” missionMain concept of “Millimetron” mission• Concept 12 m diameter deployable antenna of “Millimetron”Concept 12 m diameter deployable antenna of “Millimetron”• Astronomical instrumentsAstronomical instruments• SensitivitiesSensitivities• ConclusionsConclusions
ISSTT 2008, Groningen 3
Telescopes for Radio-astronomy Space MissionsTelescopes for Radio-astronomy Space Missions
• Main requirements and trendsMain requirements and trends• Driven by scientific objectiveDriven by scientific objective• Telescope size, diameter Telescope size, diameter
• Better sensitivity for compact sources ~DBetter sensitivity for compact sources ~D22
• Better spatial resolution ~DBetter spatial resolution ~D-1-1
• The larger the betterThe larger the better• Mirror accuracyMirror accuracy
• Tendency to observe frequencies, inaccessible from groundTendency to observe frequencies, inaccessible from ground• RF > 1 THzRF > 1 THz
• Telescope coolingTelescope cooling• Background radiation ~TBackground radiation ~T44
• Space environment allow for passive (50 K) and active coolingSpace environment allow for passive (50 K) and active cooling• 4 K dish is highly desired4 K dish is highly desired
• Large deployable apertures are neededLarge deployable apertures are needed• Ultimate mission: a free flying interferometer with large cold telescopes Ultimate mission: a free flying interferometer with large cold telescopes
(>6) (>6) FIRIFIRI• There are practicalities…There are practicalities…
ISSTT 2008, Groningen 4
Millimetron mission parameters and statusMillimetron mission parameters and status
• Frequency range: from mm wave to THz frequenciesFrequency range: from mm wave to THz frequencies• Two observing modesTwo observing modes
• Space earth VLBISpace earth VLBI• Single dish modeSingle dish mode
• Heterodyne and direct detection instruments (arrays)Heterodyne and direct detection instruments (arrays)• Aperture diameter 12 metersAperture diameter 12 meters
• ~4 m diameter central solid dish (~4 m diameter central solid dish (goalgoal 5 µm surface, 4 THz) 5 µm surface, 4 THz)• 12 m petal type deployable (12 m petal type deployable (goalgoal 10 µm RMS surface, 10 µm RMS surface,
1..2 THz)1..2 THz)• Passively cooled, 30..50 K (study active cooling possibilities)Passively cooled, 30..50 K (study active cooling possibilities)
• Mass < 4000 kgMass < 4000 kg• Orbit similar to Radioastron 300000 km apogee or L2Orbit similar to Radioastron 300000 km apogee or L2• Approved mission in Russia (Included in 10 year plan of RSA)Approved mission in Russia (Included in 10 year plan of RSA)• Now in conceptual phase, launch frame ~2017..18Now in conceptual phase, launch frame ~2017..18
ISSTT 2008, Groningen 5
Spacecraft conceptSpacecraft concept
“Navigator” spacecraft platform
Three layer deployable thermal shields
Deployable primary mirror Cold focal plane instruments (0.1…4 K)
Deployable truss
ISSTT 2008, Groningen 6
Space platform NavigatorSpace platform Navigator
Lavochkin association
ISSTT 2008, Groningen 7
Antenna optical parametersAntenna optical parameters
• Cassegrain schemeCassegrain scheme• Diameter 12 mDiameter 12 m• Secondary focus 4414.3Secondary focus 4414.3• Moveable secondary mirrorMoveable secondary mirror• Active main dish (concept) Active main dish (concept)
including laser petal position including laser petal position measurements and feed measurements and feed abck systemabck system
ISSTT 2008, Groningen 8
Radiosatron antenna construction (folded)Radiosatron antenna construction (folded)
Proton-MLauncher
ISSTT 2008, Groningen 9
Details openingDetails opening
ISSTT 2008, Groningen 10
Antenna deployment conceptAntenna deployment concept
Two 20:1 scalemodels are beingmade
ISSTT 2008, Groningen 11
Deploying sequenceDeploying sequence
ISSTT 2008, Groningen 12
Astronomical instrumentsAstronomical instruments
• Large format low spectral resolution camera (polarization Large format low spectral resolution camera (polarization sensitive)sensitive)
• Medium spectral resolution (R=1000..5000) imaging Medium spectral resolution (R=1000..5000) imaging spectrometer (similar to SPICA SAFARI)spectrometer (similar to SPICA SAFARI)
• High resolution spectrometer (similar to Herschel HIFI High resolution spectrometer (similar to Herschel HIFI instrument)instrument)
• SVLBI instruments (heterodyne, covering ALMA bands) SVLBI instruments (heterodyne, covering ALMA bands)
ISSTT 2008, Groningen 13
Low resolution spectrometerLow resolution spectrometer
• 1mm .. 0.15 mm wavelength, several channels1mm .. 0.15 mm wavelength, several channels• State of the art sensitivityState of the art sensitivity• Up to 10 kPixels for the shorter wavelength channelUp to 10 kPixels for the shorter wavelength channel• Use 12m diameter aperture up to 0.15 mm Use 12m diameter aperture up to 0.15 mm • Possibility to use central mirror for shorter wavelengthsPossibility to use central mirror for shorter wavelengths
• Specifically do not mention technologiesSpecifically do not mention technologies• NEP 10^-19 required depending on the achieved antenna NEP 10^-19 required depending on the achieved antenna
temperature temperature
• Cooling 100..300 mKCooling 100..300 mK
ISSTT 2008, Groningen 14
PhotometerPhotometer ( (SPIRE)SPIRE)
ISSTT 2008, Groningen 15
Sensitivity of photometer, 12m dish, 50KSensitivity of photometer, 12m dish, 50K
ISSTT 2008, Groningen 16
Photometer sensitivity 4m central dish, 50 KPhotometer sensitivity 4m central dish, 50 K
ISSTT 2008, Groningen 17
Photometer sensitivityPhotometer sensitivity
ISSTT 2008, Groningen 18
4K dish temperature (for reference)4K dish temperature (for reference)
1 1 0 1 0 0 1 0 0 0 1 0 40 .1
1
1 0
1 0 0
1 0 0 0
1 0 4
W a v e le ngth (m )
Det
ectio
nLi
mit
5–
1H
our(
Jy )
12 m dish , 10 m R M S, 50 K , R = 3
A L M A
JW ST M IR I
SP IC A M IR
H erschel SP IR EH erschel P A C S
SP IC A FIR SO AP
SP IC A FIR G OA L
M illim e tr o n
1 1 0 1 0 0 1 0 0 0 1 0 40 .1
1
1 0
1 0 0
1 0 0 0
1 0 4
W a v e le ngth (m )
Det
ectio
nLi
mit
5–
1H
our(
Jy )
12 m centra l dish , 10 m R M S , 4 K , R = 3
A L M A
JW ST M IR I
SP IC A M IR
H erschel SP IR EH erschel P A C S
SP IC A FIR SO AP
SP IC A FIR G OA L
M illim e tr o n
ISSTT 2008, Groningen 19
Medium resolution spectrometerMedium resolution spectrometer
• 1mm .. 0.15 mm wavelength, several channels1mm .. 0.15 mm wavelength, several channels• State of the art sensitivityState of the art sensitivity• Up to 5 kPixels for the shorter wavelength channelUp to 5 kPixels for the shorter wavelength channel• Use 12m diameter aperture up to 0.15 mm Use 12m diameter aperture up to 0.15 mm • Possibility to use central mirror for shorter wavelengthsPossibility to use central mirror for shorter wavelengths• R=1000..5000 (frequency dependent)R=1000..5000 (frequency dependent)• Technology TBDTechnology TBD
• NEP 10^-19 required depending on the achieved antenna NEP 10^-19 required depending on the achieved antenna temperature temperature
• Cooling 100…300mKCooling 100…300mK
ISSTT 2008, Groningen 20
FTSFTS ( (SPIRE)SPIRE)
ISSTT 2008, Groningen 21
Sensitivity of medium resolution spectrometerSensitivity of medium resolution spectrometer
ISSTT 2008, Groningen 22
Sensitivity of medium resolution spectrometerSensitivity of medium resolution spectrometer
ISSTT 2008, Groningen 23
Sensitivity of medium resolution spectrometerSensitivity of medium resolution spectrometer
ISSTT 2008, Groningen 24
4K dish for reference4K dish for reference
1 5 1 0 5 0 1 0 0 5 0 0 1 0 0 01 0 -2 1
1 0 -2 0
1 0 -1 9
1 0 -1 8
1 0 -1 7
1 0 -1 6
W a v e le ngth (m )
Det
ectio
nLi
mit
5–
1H
our(
Wm
-2)
12 m dish , 10 m R M S, 50 K , R = 1000
AL M A
JW ST M IR I
SP IC A M IR
Spitzer IR S
Herschel SP IR E
Herschel P AC S
SP IC A FIRSOA P
SP IC A FIR GO AL
M illim e tr o n
1 5 1 0 5 0 1 0 0 5 0 0 1 0 0 0
1 0 -2 1
1 0 -2 0
1 0 -1 9
1 0 -1 8
1 0 -1 7
1 0 -1 6
W a v e le ngth (m )
Det
ectio
nLi
mit
5–
1H
our(
Wm
-2)
12 m dish , 10 m R M S, 4 K , R = 1000
AL M A
JW ST M IR I
SP IC A M IR
Spitzer IR S
Herschel SP IR E
Herschel P AC S
SP IC A FIRSOA P
SP IC A FIR GO AL
M illim e tr o n
ISSTT 2008, Groningen 25
High resolution spectrometerHigh resolution spectrometer
• R > 10000R > 10000• Spot or continuous frequency bands 500-2000 THz for 12m Spot or continuous frequency bands 500-2000 THz for 12m
apertureaperture• Spot frequency bands up to 5 THz using central solid dishSpot frequency bands up to 5 THz using central solid dish• Small focal plane arrays for lower frequencies (LO power Small focal plane arrays for lower frequencies (LO power
limited)limited)• IF 4-12 GHzIF 4-12 GHz• Polarization !!!Polarization !!!• Conceptually based on Herschel HIFI instrumentConceptually based on Herschel HIFI instrument
• Cooling 4 KCooling 4 K
ISSTT 2008, Groningen 26
Herschel HIFIHerschel HIFI
ISSTT 2008, Groningen 27
Example of frequency distributionExample of frequency distribution
Millimetron Single-dish instrumentation
Instrument Frequency (GHz) or wavelength
Ang. res. ()
Spectral res.
Detector technology
Sensitivity TRL
Heterodyne receivers
HET-1 480 – 700 8…12 106 SIS 2x2 mixer array with multiplier LO
Tsys < 100 K 6
1100 – 1400 5…6 106 Tsys < 200 K 6
HET-2 1650 – 2000 ~3 106 HEB mixers with multiplier or QCL LO
Tsys < 500 K 6
2600 – 2700 ~2.5 106 Tsys < 700 K 4
4700 – 4800 4 (1) 106 Tsys < 1000 K 4
Far-Infrared imaging photometer/spectrometer
M-PACS 60 – 210 m 4 few 103 spectrom.
Photoconductor arrays
2 x 10-18 Wm-2 6
ISSTT 2008, Groningen 28
SensitivitiesSensitivities
0 .5 1 .0 1 .5 2 .0 2 .5 3 .0 3 .5 4 .0
1 0 -2 2
1 0 -2 1
1 0 -2 0
1 0 -1 9
1 0 -1 8
F r e q ue nc y ( T H z )
Det
ectio
nLi
mit
5–
1H
our(
Wm
-2)
R = 10000
5 quanta, 5 m R M S , 4 m5 quanta, 10 m R M S , 12 m1 quantum, 5 m R M S , 4 m1 quantum, 10 m R M S , 12 m
ISSTT 2008, Groningen 29
SVLBI instrumentsSVLBI instruments
• R > 10000R > 10000• Selected ALMA bands 500-1000 THz for 12m apertureSelected ALMA bands 500-1000 THz for 12m aperture• Spot frequency bands up to 5 THz using central solid dishSpot frequency bands up to 5 THz using central solid dish• On board data recorderOn board data recorder• On board stable referenceOn board stable reference• Fast data linkFast data link• IF 4-12 GHz (compatible to ALMA)IF 4-12 GHz (compatible to ALMA)
• Can be conceptually based on Herschel HIFI instrumentCan be conceptually based on Herschel HIFI instrument
• Cooling 4 KCooling 4 K
ISSTT 2008, Groningen 30
Instrument type
VLBI receiver
Heterodyne receiverscovering ALMA bands
Receiver VLBI-1 ALMA-1 ALMA-3 ALMA-6 ALMA-9
Frequency range
18 – 26 GHz
31.3 - 45 GHz
84-116 GHz 211-275 GHz
600-720 GHz
Detector technology
HEMT amplifier
SIS mixers, multiplier chain LO, dual pol.
Or HEMT
SIS mixers, multiplier chain LO, dual pol.
SIS mixers, multiplier chain LO, dual pol.
SIS mixers, multiplier chain LO, dual pol.
Sensitivity Tsys < 40 K < 17 K SSB < 37К SSB < 90 K SSB < 150 K DSB
TRL 6 6 6 6 6