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Experimental search for Gravitational Waves

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Title: Experimental search for Gravitational Waves


1
Experimental search for Gravitational Waves
  • Geppo Cagnoli
  • cagnoli_at_fi.infn.it
  • INFN - Firenze
  • University of Glasgow
  • Physik-Institut der Universität Zürich/ETH 28th
    June 2006

2
The GR prediction
Newtons Theory instantaneous action at a
distance
Gmn 8pTmn
Einsteins Theory information carried by
gravitational radiation at the speed of light
3
Sources of Gravitational Waves
  • Compact object binaries
  • Pulsars
  • Neutron Star internal dynamics
  • Non symmetrical supernovae
  • Cosmological gravitational waves

4
New potential sources
January 05 A swarm of 10,000 or more black holes
may be orbiting the Milky Way's supermassive
black hole, according to new results from NASA's
Chandra X-ray Observatory. This would represent
the highest concentration of black holes anywhere
in the Galaxy.
5
Detection Principles -1
  • In the reference frame of the lab (Fermis
    coordinates) the effect of GW is pure mechanical.
    The potential is
  • 3 types of detectors
  • Resonators
  • Interferometers
  • RF cavities

6
Detection Principles -2
Effect of a sinusoidal gravitational wave going
through the slideon the space-time frame and on
a circular distribution of free masses
Figure M.Lorenzini
7
Detection Principles -3
Two detectors fully developed Resonant Masses
Interferometers
Figure S. Reid
8
Theory of GW Detectors - 1
Detector
9
First attempt of buildinga resonant detector
Joseph Weber(1960)
Resonant barsuspended in the middle
Piezoelectrictransducers
10
The Band Width of a resonant detector
11
Resonant detectors today
GW bursts excite the resonances of the test masses
Capacitive SQUIDor optical readout
12
A capacitive Read-out systemof a resonant
detector
13
(No Transcript)
14
Interferometric detectorsthe concept
  • Monitoring the distances between free-flying
    masses with laser interferometer
  • The background noise comes from the readout
    and from the internal motion of the masses

15
A bit of history
  • Gertsenshtein M E and Pustovoit V I 1962 Sov.
    Phys.JETP 16 433
  • Moss G E, Miller L R and Forward R L 1971 Appl.
    Opt. 10 2495b
  • Weiss R 1972 Q. Prog. Rep. Res. Lab. Electron.
    105 54

16
The Band Width of an interferometric detector
17
Interferometers today - 1
  • End mirrors positioned in theDark Fringe
    condition laser beam is frequency modulated,
    the sidebands are detected
  • Multiple bouncingphase accumulationlaser power
    increasesfrom 20W to 1kW
  • Power recycling number ofphotons in the
    interferometerincreases
  • Signal recyclingjust the side bands are
    reflectedback in the interferometerGEO600 is
    the onlydetector that uses thistechnique to
    enhance the detector response in a narrow band

Pendulumsuspensions
Beamsplitter
Photodiode
Laser
18
Interferometers today - 2
Pendulumsuspensions
Beamsplitter
Photodiode
Laser
19
Interferometers today - 3
Pendulumsuspensions
Beamsplitter
Photodiode
The optics and suspensions are in vacuum to
minimize fluctuation of index of refraction
Laser
20
Interferometers today - 4
600 m
TAMA
4 2 km
300 m
AIGO
4 km
21
Real data from LIGO
22
Real data from GEO600
10 -17
Displacement m
10 -18
10 -19
100
Hz
1000
23
Real data from Virgo
24
Detectors of 1st Generation
h
Pulsars
Hz 1/2
Supernovae
NSvibration
BUT THEEVENT RATEIS TOO LOW !! 1 EVENT/3
YRS MOST OPTIMISTICCASE
25
Future Detectors of Gravitational Waves
  • DUAL
  • Nested hollow cylinder resonant detector
  • AURIGA collaboration
  • Construction planned starting on 2009
  • Ad. LIGO, Ad. Virgo and GEO HF
  • 2nd generation interferometers
  • Virgo GEO600 collaboration
  • Commissioning starts on 2009
  • 3rd Generation Interferometer
  • Cryogenic and underground interferometer
  • Construction envisaged by 2014

26
DUAL the concept
read-out the differential deformations of two
nested resonators
The inner resonator is driven below resonance
The outer resonator is driven above resonance
p Phase difference
5.0 kHz
useful GW band
27
DUAL performance
M. Bonaldi et al. Phys. Rev. D 68 102004 (2003)
Mo Dual 16.4 ton height 3.0m 0.94m SiC
Dual 62.2 ton height 3.0m 2.9m
Antenna pattern like 2 IFOs colocated and
rotated by 45
Q/T2x108 K-1
28
Real data from Virgo
CONTROL RELATED NOISE
29
Readout noise shot noise
  • A fundamental limit to phase measurement is due
    to the quantum nature of light
  • Phase measurements to a level of 10 -13 rad
    require about 1 MW of laser power in the optical
    cavities
  • But more power more fluctuating radiation
    pressure P1 MW ?? F3 mN ?? dF1.5

DN Dj 1/2
fN
30
Readout noiseThe Standard Quantum Limit
  • For a simple Michelson interferometer (GEO HF
    parameters)

RomanSchnabelMPG-AEI Hannover
10-21
Quantum noise with increased laser power (x100)
10-23
1
100
Frequency Hz
31
Beyond the SQL Squeezed Light
  • In one representation of the EM field the two
    orthogonal states are the Amplitude Quadrature
    X1 and the Phase Quadrature X2

RomanSchnabelMPG-AEI Hannover
32
Beyond the SQL Squeezed Light
  • In one representation of the EM field the two
    orthogonal states are the Amplitude Quadrature
    X1 and the Phase Quadrature X2

RomanSchnabelMPG-AEI Hannover
33
Beyond the SQL Squeezed Light
10-21
RomanSchnabelMPG-AEI Hannover
Quantum limit onphase measurement
Radiation pressure noise
SQL
10-22
1
100
Frequency Hz
34
Squeezed light demonstrations
35
Intermediate frequencies
From the realm of Quantum to the realm of
Statistical Physics
36
Thermal noise
  • Non isolated system shows uncorrelated
    fluctuations of volume and temperature
  • The equipartition principle states that each
    observable has a mean energy equal to kBT/2
  • The observable
  • Optical readout part of the mirror sensed by the
    laser
  • Capacitive readout the average position of the
    capacitor plates

37
Thermal noise reduction strategy
  • Linear systems thermal equilibrium
  • Each dynamic variable ltEgt kT
  • Fluctuation-Dissipation theorem

Lower T ?? Lower thermal noise
Thermal noise for Damped HarmonicOscillator
Lower dissipation ?? Lower thermal noise
38
The most severe limit for IFOsthermal noise
from the coatings
  • Alternate layers of transparent materials with
    different index of refraction
  • Impedance mismatch andinterference produce
    highcoefficient of reflectivity
  • Its structure is not compact as the
    substrateDeposition with DIBS
  • 10 mm of coating produces morethermal noise than
    10 cm of substrate

QUANTUM
COATINGS
EGO
SUBSTRATES
39
Suspensions at room temperature
  • Best materialsilica (SiO2)
  • Silicate bonding
  • Tested on GEO600

40
Silicon for mirrors and suspensions at low T
  • Thermal expansion null at 124K and 18K ? main
    source of thermal noise is ruled out
  • High thermal conductivity
  • Monocrystal ingots up to 45cm diameter
  • Possibility of monolithic suspensions
  • Diffractive as well as transmissive
    interferometry allowed

k
5000
2.5e-6
a
41
Earth related noise - 1
  • Test masses have to behave like free flying
    objects, yet they have to be suspended against
    gravity
  • Seismic motion always present has to be filtered

42
Earth related noise - 2Isolation short-circuit
The Newtonian noisewill be dominant below 10 Hz
for cryogenic detectors Surface waves
die exponentially with depth GO UNDERGROUND!
Figure M.Lorenzini
43
Further considerations
  • Building the most perfect inertial reference
    system
  • A system subjected to the quantum problem of
    measurement
  • All the fundamental parameters of the detector
    have to be CONTROLLED without introducing a
    significant noise

44
Detector Generations
Distance Rate
NS-NS 14 Mpc 1/30ce 1/3yr
NS-BH 29 Mpc 1/25ce 1/2yr
BH-BH 67 Mpc 1/6ce 3/yr



h
Hz 1/2
NS-NS 240 Mpc 3/yr 4/day
NS-BH 500 Mpc 1/yr 6/day
BH-BH Z0.3 1/month 30/day
45
NS-NS coalescence range
BH-BH coalescence range
46
Beyond Earth based detectorsLISA
LISA
47
A collaborative ESA NASA mission
  • Cluster of 3 S/C in heliocentric orbit
  • Trailing the earth by 20 (50 Mio km)
  • Equilateral triangle with 5 Mio km arms
  • Inclined against ecliptic by 60

48
The spacecraft
  • LISA needs a purely gravitational orbit
  • Test masses have to be shielded from solar
    wind
  • Capacitive sensing of the test masses
  • Feedback loop to propulsion
  • FEEP thrusters with micro-Newton thrust

49
The Payload
50
LISA technology demonstration
10-12
10-13
10-14
10-15
51
LISA Path Finder Mission
Only one S/C with two test masses is needed
Testing Inertial sensor Charge
management Thrusters Drag-free control Low
frequency laser metrology  
52
LISA sensitivity curve
LISA will see all the compact white-dwarf and
neutron-star binaries in the Galaxy. (Schutz)
53
Conclusions
A new way to observe the Universe
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