Pre-Phase A Report - Lisa - Nasa

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186 References [120] R. Hellings, G. Giampieri, L. Maleki, M. Tinto, K. Danzmann, J. Hough, D. Robertson, Heterodyne laser tracking at high Doppler rates, Opt. Commun. 124, (1996) 313–320 . [121] R.T. Stebbins, P.L. Bender, W.M. Folkner, LISA data acquisition, Class. Quantum Grav. 13 (1996) A285–A289 . [122] C. Bartoli, H. von Rohden, S. Thompson, J. Blommers, A Liquid Caesium Field Ion Source for Plasma Propulsion, J. Phys. D: Appl. Phys. 17 (1984) 2473–2483. [123] B.T.C. Zandbergen, FEEP: the ESTEC Liquid Caesium Field Ion Source. An Investigative <strong>Report</strong>, Thesis TU Delft, June 1984. [124] C. Bartoli, J. González, G. Saccoccia, M. Andrenucci, S. Marcuccio, A. Genovese, Space-Borne Astronomical Gravity wave Interferometer Mission (SAGITTARIUS): the FEEP option, IEPC–93–016. [125] J. González, G. Saccoccia, H. von Rohden, Field Emission Electric Propulsion: Experimental Investigations on Microthrust FEEP Thrusters, IEPC–93–157. [126] M. Andrenucci, S. Marcuccio, L. Spagli, A. Genovese and F. Repola, Experimental Study of FEEP Emitter Starting Characteristics, IEPC–91–104. [127] A. Ciucci, G. Genuini and M. Andrenucci, Experimental Investigation of Field Emission Electrostatic Thrusters, IEPC–91–103. [128] R. Schmidt, H. Arends et al., A novel medium-energy ion emitter for active spacecraft potential control, Rev. Sci. Instrum. 64 (1993). [129] M. Fehringer, F. Rüdenauer and W. Steiger, Space-Proven Indium Liquid Metal Field Ion Emitters for Ion Microthruster Applications, 33rd AIAA Joint Propulsion Conference, Seattle, WA (1997), AIAA 97-3057. 3-3-1999 9:33 Corrected version 2.08
List of Acronyms – and other abbreviations and mission names 1553 (standardised interface bus) AC Alternating Current ACS Attitude Control System Ada (a programming language) AFRP Aramid Fibre Reinforced Plastic AO Announcement of Opportunity ARC Austrian Research Centre, Seibersdorf ARISTOTELES Applications and Research Involving Space Techniques Observing The Earth field from Low-Earth orbiting Satellite ASCA – satellite name – ASI Agenzia Spaziale Italiano ASTRE Accelerometre Spatial TRiaxial Electrostatique AU Astronomical Unit : distance Sun–Earth AURIGA Antenna Ultracriogenica Risonante per l’Indagine Gravitazionale Astronomica : cryogenic resonant-mass antenna, Legnaro, Italy BH Black Hole BOL Begin Of Lifetime C (a programming language) C++ (an object-oriented programming language) C&DH Command and Data Handling CAD Computer Aided Design CAESAR Capacitive And Electrostatic Sensitive Accelerometer Reference CASSINI – NASA space mission (1997) to orbit Saturn – CCSDS Consultative Committee for Space Data Systems, telemetry standard CD-ROM Compact Disk – Read Only Memory CERN Centre Européen de la Recherche Nucléaire CFRP Carbon Fibre Reinforced Plastic CHAMP – German geodetic satellite – CLUSTER-II – ESA/NASA space mission (2000), 4 s/c to be launched on Ariane 5 – CNES Centre National d’Etude Spatiales (France) CO Carbon-Oxygen COBE COsmic Background Explorer COLUMBIA – NASA spaceshuttle– COLUMBUS – ESA space mission, to fly on NASA shuttle, 1996 – COSPAR Committee On SPAce Research CPU Central Processing Unit Corrected version 2.08 187 3-3-1999 9:33
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LISA Laser Interferometer Space Ant
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LISA Laser Interferometer Space Ant
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Foreword The first mission concept
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The result of the Team-X study was
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Contents Foreword iii Executive Sum
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Contents ix 4.2.3 Acceleration nois
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Contents xi 9 Science and Mission O
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Executive Summary 1 Executive Summa
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Executive Summary 3 Complementarity
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Mission Summary 5 LISA Mission Summ
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Chapter 1 Scientific Objectives By
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1.1 Theory of gravitational radiati
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1.2 Low-frequency sources of gravit
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Chapter 2 Different Ways of Detecti
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2.2 Ground-based detectors 39 2.2 G
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2.2 Ground-based detectors 41 Count
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2.4 Spacecraft tracking 43 2.4 Spac
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2.7 Heliocentric versus geocentric
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2.8 The LISA concept 47 telescopes
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2.8 The LISA concept 49 Figure 2.6
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2.8 The LISA concept 51 seem rather
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Chapter 3 Experiment Description 3.
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3.1 The interferometer 55 Fiber to
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3.1 The interferometer 57 3.1.4 Sys
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3.1 The interferometer 59 Figure 3.
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3.1 The interferometer 61 3.1.6 Las
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3.1 The interferometer 63 signal sh
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3.1 The interferometer 65 for a sin
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3.2 The inertial sensor 67 design (
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3.2 The inertial sensor 69 and the
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3.2 The inertial sensor 71 Figure 3
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3.2 The inertial sensor 73 sufficie
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3.3 Drag-free/attitude control syst
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3.3 Drag-free/attitude control syst
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Chapter 4 Measurement Sensitivity 4
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4.1 Sensitivity 81 averaged transfe
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4.2 Noises and error sources 83 The
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4.2 Noises and error sources 85 Tab
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4.2 Noises and error sources 87 cod
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4.2 Noises and error sources 89 cha
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4.2 Noises and error sources 91 fre
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4.2 Noises and error sources 93 ele
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4.2 Noises and error sources 95 is
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4.2 Noises and error sources 97 and
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4.2 Noises and error sources 99 Eq.
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4.3 Signal extraction 101 here that
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4.3 Signal extraction 103 phase loc
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4.4 Data analysis 105 • LISA obse
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4.4 Data analysis 107 for ground-ba
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4.4 Data analysis 109 that are defi
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4.4 Data analysis 111 with the phas
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4.4 Data analysis 113 density Sn(f)
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4.4 Data analysis 115 box (in stera
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4.4 Data analysis 117 LISA’s dist
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Chapter 5 Payload Design 5.1 Payloa
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5.2 Payload structural components 1
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5.2 Payload structural components 1
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5.4 Mass estimates 125 5.4 Mass est
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5.7 Thermal analysis 127 the Y-shap
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5.8 Telescope assembly 129 surface
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5.9 Payload processor and data inte
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5.9 Payload processor and data inte
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