- Page 1: LISA Laser Interferometer Space Ant
- Page 5 and 6: LISA Mission Summary Objectives: Pa
- Page 7 and 8: Foreword The first mission concept
- Page 9 and 10: Foreword The ESA personnel from the
- Page 11 and 12: Contents Mission Summary Table Fore
- Page 13 and 14: Contents 5.6.3 On-board frequency r
- Page 15 and 16: Contents 9.5.2 Thermal design . . .
- Page 17 and 18: Contents A.1.1 Overview . . . . . .
- Page 19 and 20: Executive Summary The primary objec
- Page 21 and 22: Executive Summary Figure 1 LISA Sen
- Page 23 and 24: Executive Summary radiation pressur
- Page 25 and 26: 1 Scientific Objectives By applying
- Page 27 and 28: 1.1 Theory of gravitational radiati
- Page 29 and 30: 1.1 Theory of gravitational radiati
- Page 31 and 32: 1.1 Theory of gravitational radiati
- Page 33 and 34: 1.1 Theory of gravitational radiati
- Page 35 and 36: ' 798;: < 8>=@? 6 6 5 02143 3 ¡
- Page 37 and 38: 1.2 Low-frequency sources of gravit
- Page 39 and 40: 1.2 Low-frequency sources of gravit
- Page 41 and 42: 1.2 Low-frequency sources of gravit
- Page 43 and 44: 1.2 Low-frequency sources of gravit
- Page 45 and 46: 1.2 Low-frequency sources of gravit
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2 Different Ways of Detecting Gravi
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2.2 Ground-based detectors light so
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2.3 Pulsar timing construction, and
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2.6 Early concepts for a laser inte
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2.7 Heliocentric versus geocentric
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3 The LISA Concept - An Overview Th
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3.3 The three LISA spacecraft 60 o
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3.4 The payload Support cylinder Pr
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3.5 Lasers 3.5 Lasers Lasers have e
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3.9 System options and trade-off cy
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3.10 Summary tables Table 3.2 Optic
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4 Measurement Sensitivity 4.1 Inter
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4.2 Noises and error sources 4.2 No
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4.2 Noises and error sources Table
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4.2 Noises and error sources Table
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5 The Interferometer 5.1 Introducti
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5.3 Interferometric layout Support
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5.3 Interferometric layout a refere
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5.3 Interferometric layout
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5.5 Laser system Component Efficien
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5.5 Laser system 5.5.2 Laser system
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5.6 Laser performance phase of the
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5.7 Beam pointing an allowed phase
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5.7 Beam pointing 3RLQW$KHDG$QJO
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5.8 Thermal stability path-length v
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6 Inertial Sensor and Drag-Free Con
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6.1 The inertial sensor configurati
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6.1 The inertial sensor Figure 6.4
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6.1 The inertial sensor laboratory
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6.2 Drag-free/attitude control syst
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6.3 Accelerations directly affectin
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7 Signal Extraction and Data Analys
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7.2 Frequency-domain cancellation o
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7.4 Alternative laser-phase and opt
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7.4 Alternative laser-phase and opt
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7.4 Alternative laser-phase and opt
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7.4 Alternative laser-phase and opt
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7.4 Alternative laser-phase and opt
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7.4 Alternative laser-phase and opt
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7.5 Data analysis from ground-based
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7.5 Data analysis 7.5.1.4 Parameter
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7.5 Data analysis 7.5.2.2 The beam-
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7.5 Data analysis 7.5.2.4 The LISA
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7.5 Data analysis where the symmetr
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7.5 Data analysis f [Hz] Case ∆ I
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7.5 Data analysis • possible cosm
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8 Payload Design 8.1 Payload struct
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8.2 Payload structural components r
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8.4 Payload thermal requirements It
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8.6 Thermal analysis 8.6 Thermal an
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8.7 Telescope assembly would have t
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8.8 Payload processor and data inte
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9 Spacecraft Design 9.1 The Pre-Pha
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9.2 Spacecraft subsystem design 9.1
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9.2 Spacecraft subsystem design 9.2
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9.3 The revised spacecraft design 9
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9.3 The revised spacecraft design a
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9.3 The revised spacecraft design s
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9.4 Structure and Mechanisms • A
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9.4 Structure and Mechanisms Stiffe
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9.5 Thermal control spindles will t
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9.5 Thermal control tube and the re
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9.5 Thermal control be seen that in
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9.5 Thermal control Mechanisms : An
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9.6 Spacecraft electrical subsystem
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9.6 Spacecraft electrical subsystem
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9.6 Spacecraft electrical subsystem
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9.6 Spacecraft electrical subsystem
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9.6 Spacecraft electrical subsystem
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9.6 Spacecraft electrical subsystem
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9.6 Spacecraft electrical subsystem
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9.7 Micronewton ion thrusters opmen
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9.7 Micronewton ion thrusters • I
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9.7 Micronewton ion thrusters Figur
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9.8 Mass and power budgets Subsyste
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10 Mission Analysis 10.1 Orbital co
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10.4 Orbit configuration stability
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10.5 Orbit determination and tracki
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10.6 Launch phase lengths are deter
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10.7 Operational orbit injection an
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10.8 Evolution of the operational o
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10.8 Evolution of the operational o
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11 Technology Demonstration in Spac
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11.1 SMART2 technology demonstratio
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11.3 SMART2 technologies 11.3 SMART
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11.4 SMART2 satellite design 11.4.1
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12 Science and Mission Operations 1
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12.3 Operating modes 12.3 Operating
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12.4 Operational strategy contain t
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12.5 Mission phases The central ite
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12.6 Operating modes and mode trans
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12.6 Operating modes and mode trans
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12.7 Ground segment will perform da
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13 International Collaboration, Man
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13.4 Archiving mission with NASA (p
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Appendix A.1 Detailed Noise Analysi
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A.1 Detailed Noise Analysis 0.1 0.0
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A.1 Detailed Noise Analysis Bench A
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A.1 Detailed Noise Analysis Figure
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A.1 Detailed Noise Analysis 2π ⎛
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A.1 Detailed Noise Analysis The gen
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A.1 Detailed Noise Analysis equatio
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A.1 Detailed Noise Analysis reached
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A.1 Detailed Noise Analysis noise c
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A.1 Detailed Noise Analysis 100000.
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A.1 Detailed Noise Analysis The mos
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A.1 Detailed Noise Analysis A.1.2.9
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A.1 Detailed Noise Analysis A.1.3 R
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A.1 Detailed Noise Analysis Table A
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A.1 Detailed Noise Analysis Table A
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A.1 Detailed Noise Analysis 2. 10 -
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A.2 Proof-mass charging by energeti
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A.2 Proof-mass charging by energeti
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A.2 Proof-mass charging by energeti
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A.2 Proof-mass charging by energeti
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A.2 Proof-mass charging by energeti
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A.3 Disturbances due to minor bodie
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A.3 Disturbances due to minor bodie
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A.4 Alternative Proof-Mass Concepts
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A.4 Alternative Proof-Mass Concepts
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A.5 Laser Assembly Concepts A.5 Las
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A.5 Laser Assembly Concepts Figure
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A.5 Laser Assembly Concepts Figure
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A.5 Laser Assembly Concepts • Pum
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A.5 Laser Assembly Concepts Figure
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A.6 Telescope A.6 Telescope A.6.1 T
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A.6 Telescope have been polished us
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A.6 Telescope • good compressive
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A.6 Telescope pointing bias and jit
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A.6 Telescope The Dall-Kirkham desi
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A.7 Line-of-Sight Orientation Mecha
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A.7 Line-of-Sight Orientation Mecha
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A.7 Line-of-Sight Orientation Mecha
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A.7 Line-of-Sight Orientation Mecha
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A.7 Line-of-Sight Orientation Mecha
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A.7 Line-of-Sight Orientation Mecha
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References [1] LISA Study Team, LIS
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References [37] G. Nelemans, S.F. P
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References [85] A. Abramovici et al
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References [116] T.J. Sumner and G.
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References [150] J.A. Halbleib, R.P
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Acronyms CERN Conseil Européen de
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Acronyms JILA Joint Institute for L
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Acronyms RF Radio Frequency RFC Rad
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Earth 5 × 10 6 km 1 AU 20 o 60 o S