LISA October 3, 2005 LISA Laser Interferometer Space Antenna Gravitational Physics Program Technical implications Jo van den Brand NIKHEF – Staff Meeting, January 2006
LISA VIRGO & Lisa – Technical activities Linear alignment of Virgo – Keep mirrors and input beam aligned Monolithic suspension of Virgo mirrors – Reduce thermal noise Recycling mirror for Virgo+ – Improve mirror suspension Lisa electronics – Drag-free control readout
LISA Linear alignment of VIRGO interferometer N W EOM Phase modulation of input beam Demodulation of photodiode signals at different output beams – => longitudinal error signals Quadrant diodes in output beams – => Alignment information – (differential wavefront sensing) Anderson-Giordano technique – 2 quadrant diodes after arm cavities
LISA Can have 1 normal diode and 2 quadrant diodes at each output port Detection
LISA Linear alignment setup
LISA Present Virgo noise budget Control noise
LISA Present situation Frascati group is leaving Virgo – Since 01/2006 Frascati’s responsibilities – Original design of alignment system –Strategy, optics, prototype experiments, … – Design & realization of electronics Problem – Continue support for alignment electronics – Make new modules / spare modules – Continue development for new requirements
LISA Developments Present developments – More modules needed –Installation of 9 th quadrant diode (maybe 10 th ) –Spares needed – New Annecy local oscillator boards, compatible with alignment –Phase shifters for standard photodiodes Possible developments – Substitute Si diodes with InGaAs diodes –Better quantum efficiency –Lower bias voltage –=> higher power capability lower noise Reduction of electronics noise Better preamplifier: 5 pA/rtHz -> 1.6 pA/rtHz (?) DC signals: pre-amplification / pre-shaping – Fast quadrant centering system –(Napoli is working on that) –LA noise limits sensibility (especially at low frequencies)
LISA QD electronics demodulator phase shifter Quadrant diode box Manpower estimate ~ 3FTE from electronics group
LISA Virgo – local control of mirrors Local control of mirrors Present accuracy about 1 micron Feedback systems induce noise Possible application for RASNIC
LISA VIRGO Optical Scheme Laser 20 W Input Mode Cleaner (144 m) Power Recycling 3 km long Fabry-Perot Cavities Output Mode Cleaner (4 cm)
LISA Virgo – inside the central building
LISA Mirror suspension High quality fused silica mirrors 35 cm diameter, 10 cm thickness, 21 kg mass Substrate losses ~1 ppm Coating losses <5 ppm Surface deformation ~l/100
Superattenuators Possible contributions: Virgo+ will use monolythic suspension Input-mode cleaner suspension
LISA Fused silica fibers Bonded to mirror Reduce thermal noise Needed for Virgo+ Realized by GEO600 Silicate (Hydroxy- Catalysis) Bonding Weld Monolithic suspension
LISA Input mode cleaner Mode cleaner cavity: filters laser noise, select TEM00 mode Input beam Transm. beamRefl. beam
LISA LISA - drag free control SRON Test equipment for position sensor read- out electronics in on-ground tests of the satellite system Simulation software modules of the position sensors, used in system simulations TNO-TPD Test equipment of the Laser Optical Bench Decaging Mechanism (TBC) Bradford Engineering Cold Gas propulsion (TBC)
LISA LISA key technology Test-mass position sensing: Capacitive sensing. Drag-Free control. FEEP micro-Newton thrusters. NIKHEF and SRON develop ASICS for electronic readout of all LISA signals Low noise, high resolution ADCs NIKHEF 2 – 3 ASIC designers + 2 FTE support
LISA Summary Linear alignment of Virgo – 3 FTE electronics Monolithic suspension of Virgo mirrors – 2 FTE EA Recycling mirror for Virgo+ – 2 FTE EA Lisa electronics – 2 – 3 ASICS designers – 2 FTE support
LISA Optimized alignment noise budget Maximized power Optimized mirror centering (0.2 mm)
LISA Scheme of LA electronics ADC noise Preamp. noise Shot noise Low-pass filter AC: Gain 200 DC: Gain 1 diff. sig. non-diff.sig. Non-optimal treatment of DC signals dominated by ADC noise (but were not foreseen as error signals) VME QD box