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The LISA Pathfinder interferometry-hardware and system testing

delete2011-04-19
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OA
AI
H
H. Audley *
K
K. Danzmann
A
Antonio García Marín
G
Gerhard Heinzel
A
A. Monsky
M
M. Nofrarías
F
Frank Steier
D
Domenico Gerardi
R
R. Gerndt
G
Gerald Hechenblaikner
P
Peter Luetzow-Wentzky
W
Wand, V.
M
M. Armano
G
G. Auger
M
M. Benedetti
C
C Boatella
J
J. Bogenstahl
D
D. Bortoluzzi
P
Paolo Bosetti
M
M Caleno
A
A. Cavalleri
M
M Cesa
M
M. Chmeissani
G
G. Ciani
A
A Conchillo
G
G. Congedo
I
I. Cristofolini
M
M Cruise
F
Fabrizio De Marchi
I
I. Diepholz
G
George Dixon
R
R. Dolesi
J
Jorge Fauste
L
L. Ferraioli
D
D Fertin
W
Walter Fichter
E
E. D. Fitzsimons
M
M. Freschi
C
C García Marirrodriga
L
L. Gesa
F
F. Gibert
D
D. Giardini
C
C. Grimani
B
B. Guillaume
F
Felipe Guzmán
I
I. Harrison
M
M. Hewitson
D
D. Hollington
J
J. Hough
D
D. Hoyland
M
M. Hueller
J
J Huesler
O
Olivier Jeannin
O
O. Jennrich
P
P. Jetzer
C
C. J. Killow
X
Xavier Llamas
I
I Lloro
A
A Lobo
R
R. Maarschalkerweerd
S
S. C. Madden
D
D. Mance
I
I Mateos
P
P. W. McNamara
J
João Mendes
E
E Mitchell
D
Davide Nicolini
D
Daniele Nicolodi
F
F. Pedersen
M
M. Perreur-Lloyd
A
A. Perreca
E
E. Plagnol
P
P. Prat
G
G D Racca
B
B Rais
J
J. Ramos-Castro
J
J. Reiche
J
J.A. Romera Perez
D
D. I. Robertson
H
H Rozemeijer
J
Jose Sanjuán
M
M Schulte
D
D. Shaul
L
L. Stagnaro
S
Stein Strandmoe
T
T. J. Sumner
A
Alasdair Taylor
D
D. Texier
C
C. Trenkel
D
D Tombolato
S
S. Vitale
G
G Wanner
H
H. Ward
S
S. Waschke
P
Peter Wass
W
W. J. Weber
P
P. Zweifel
DOI:10.1088/0264-9381/28/9/094003delete
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摘要

摘要

En 中文
Preparations for the LISA Pathfinder mission have reached an exciting stage. Tests of the engineering model (EM) of the optical metrology system have recently been completed at the Albert Einstein Institute, Hannover, and flight model tests are now underway. Significantly, they represent the first complete integration and testing of the space-qualified hardware and are the first tests on an optical system level. The results and test procedures of these campaigns will be utilized directly in the ground-based flight hardware tests, and subsequently during in-flight operations. In addition, they allow valuable testing of the data analysis methods using the MATLAB-based LTP data analysis toolbox. This paper presents an overview of the results from the EM test campaign that was successfully completed in December 2009.
Keyword:
LTP INTERFEROMETER
PHASEMETER
MISSION
NOISE
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errArmano, M.; Benedetti, M.; Bogenstahl, J.; Bortoluzzi, D.; Bosetti, P.; Brandt, N.; Cavalleri, A.; Ciani, G.; Cristofolini, I.; Cruise, A. M.; Danzmann, K.; Diepholz, I.; Dixon, G.; Dolesi, R.; Fauste, J.; Ferraioli, L.; Fertin, D.; Fichter, W.; Freschi, M.; Garcia, A.; Garcia, C.; Grynagier, A.; Guzman, F.; Fitzsimons, E.; Heinzel, G.; Hewitson, M.; Hollington, D.; Hough, J.; Hueller, M.; Hoyland, D.; Jennrich, O.; Johlander, B.; Killow, C.; Lobo, A.; Mance, D.; Mateos, I.; McNamara, P. W.; Monsky, A.; Nicolini, D.; Nicolodi, D.; Nofrarias, M.; Perreur-Lloyd, M.; Plagnol, E.; Racca, G. D.; Ramos-Castro, J.; Robertson, D.; Sanjuan, J.; Schulte, M. O.; Shaul, D. N. A.; Smit, M.; Stagnaro, L.; Steier, F.; Sumner, T. J.; Tateo, N.; Tombolato, D.; Vischer, G.; Vitale, S.; Wanner, G.; Ward, H.; Waschke, S.; Wand, V.; Wass, P.; Weber, W. J.; Ziegler, T.; Zweifel, P.
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