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LISA Pathfinder micronewton cold gas thrusters: In-flight characterization

Authors :
Nikolaos Karnesis
N. Korsakova
Jacob Slutsky
Valerio Ferroni
Daniele Vetrugno
Davor Mance
S. Paczkowski
D. Texier
Henri Inchauspe
G. Dixon
Ivan Lloro
D. Hoyland
Luigi Ferraioli
M. de Deus Silva
P. Pivato
L. Wissel
Ignacio Mateos
J. Grzymisch
Ph. Jetzer
P. Zweifel
Antonella Cavalleri
T. J. Sumner
L. Liu
N. Meshksar
Daniele Bortoluzzi
L. Mendes
Peter Wass
E. Castelli
F. Rivas
E. D. Fitzsimons
Pierre Binétruy
Lluis Gesa
S. Vitale
Heather Audley
F. Martin-Porqueras
R. Giusteri
J. Martino
A. M. Cruise
Michele Armano
R. Maarschalkerweerd
D. I. Robertson
A. Wittchen
Antoine Petiteau
Paul McNamara
Daniel Hollington
Gudrun Wanner
Miquel Nofrarías
Juan Ramos-Castro
M. Freschi
Catia Grimani
Carlos F. Sopuerta
Christian J. Killow
J. Baird
M. Hueller
Oliver Jennrich
Rita Dolesi
M. Born
Eric Plagnol
Domenico Giardini
J. A. Lobo
James Ira Thorpe
Ingo Diepholz
José F. F. Mendes
J. Reiche
A. Cesarini
G. Russano
M. Hewitson
W. J. Weber
L. Martin-Polo
H. Ward
I. Harrison
Michael Perreur-Lloyd
J. P. López-Zaragoza
Karsten Danzmann
Ferran Gibert
B. Kaune
Víctor S. Martín
Gerhard Heinzel
AstroParticule et Cosmologie (APC (UMR_7164))
Institut National de Physique Nucléaire et de Physique des Particules du CNRS (IN2P3)-Centre National de la Recherche Scientifique (CNRS)-Commissariat à l'énergie atomique et aux énergies alternatives (CEA)-Observatoire de Paris
PSL Research University (PSL)-PSL Research University (PSL)-Université Paris Diderot - Paris 7 (UPD7)
LISA Pathfinder
Observatoire de Paris
PSL Research University (PSL)-PSL Research University (PSL)-Université Paris Diderot - Paris 7 (UPD7)-Commissariat à l'énergie atomique et aux énergies alternatives (CEA)-Institut National de Physique Nucléaire et de Physique des Particules du CNRS (IN2P3)-Centre National de la Recherche Scientifique (CNRS)
Universitat Politècnica de Catalunya. Departament d'Enginyeria Electrònica
Commissariat à l'énergie atomique et aux énergies alternatives (CEA)-Institut National de Physique Nucléaire et de Physique des Particules du CNRS (IN2P3)-Observatoire de Paris
Université Paris sciences et lettres (PSL)-Université Paris sciences et lettres (PSL)-Université Paris Diderot - Paris 7 (UPD7)-Centre National de la Recherche Scientifique (CNRS)
Université Paris sciences et lettres (PSL)-Université Paris sciences et lettres (PSL)-Commissariat à l'énergie atomique et aux énergies alternatives (CEA)-Université Paris Diderot - Paris 7 (UPD7)-Centre National de la Recherche Scientifique (CNRS)-Institut National de Physique Nucléaire et de Physique des Particules du CNRS (IN2P3)
Source :
Phys.Rev.D, Phys.Rev.D, 2019, 99 (12), pp.122003. ⟨10.1103/PhysRevD.99.122003⟩, Recercat. Dipósit de la Recerca de Catalunya, instname, UPCommons. Portal del coneixement obert de la UPC, Universitat Politècnica de Catalunya (UPC), Physical Review D, Physical Review D, American Physical Society, 2019, 99 (12), pp.122003. ⟨10.1103/PhysRevD.99.122003⟩
Publication Year :
2019
Publisher :
HAL CCSD, 2019.

Abstract

International audience; The LISA Pathfinder (LPF) mission has demonstrated the ability to limit and measure the fluctuations in acceleration between two free falling test masses down to sub-femto-g levels. One of the key elements to achieve such a level of residual acceleration is the drag free control. In this scheme the spacecraft is used as a shield against any external disturbances by adjusting its relative position to a reference test mass. The actuators used to move the spacecraft are cold gas micropropulsion thrusters. In this paper, we report in-flight characterization of these thrusters in term of noise and artefacts during science operations using all the metrology capabilities of LISA Pathfinder. Using the LISA Pathfinder test masses as an inertial reference frame, an average thruster noise of ∼0.17 μN/Hz is observed and decomposed into a common (coherent) and an uncorrelated component. The very low noise and stability of the onboard metrology system associated with the quietness of the space environment allowed the measurement of the thruster noise down to ∼20 μHz, more than an order of magnitude below any ground measurement. Spectral lines were observed around ∼1.5 mHz and its harmonics and around 55 and 70 mHz. They are associated with the cold gas system itself and possibly to a clock synchronization issue. The thruster noise-floor exhibits an excess of ∼70% compared to characterization that have been made on ground on a single unit and without the feeding system. However this small excess has no impact on the LPF mission performance and is compatible with the noise budget for the upcoming LISA gravitational wave observatory. Over the whole mission, nominal, and extension, the thrusters showed remarkable stability for both the science operations and the different maneuvers necessary to maintain LPF on its orbit around L1. It is therefore concluded that a similar cold gas system would be a viable propulsion system for the future LISA mission.

Details

Language :
English
ISSN :
15507998, 15502368, and 24700010
Database :
OpenAIRE
Journal :
Phys.Rev.D, Phys.Rev.D, 2019, 99 (12), pp.122003. ⟨10.1103/PhysRevD.99.122003⟩, Recercat. Dipósit de la Recerca de Catalunya, instname, UPCommons. Portal del coneixement obert de la UPC, Universitat Politècnica de Catalunya (UPC), Physical Review D, Physical Review D, American Physical Society, 2019, 99 (12), pp.122003. ⟨10.1103/PhysRevD.99.122003⟩
Accession number :
edsair.doi.dedup.....7bd9017b41dfbb20c9fbe34b011cd8dc