Laser Ranging Interferometer for GRACE follow-on

Research output: Chapter in book/report/conference proceedingConference contributionResearchpeer review

Authors

  • Gerhard Heinzel
  • Benjmin Sheard
  • Nils Brause
  • Karsten Danzmann
  • Marina Dehne
  • Oliver Gerberding
  • Christoph Mahrdt
  • Vitali Müller
  • Daniel Schütze
  • Gunnar Stede
  • William Klipstein
  • William Folkner
  • Robert Spero
  • Kolja Nicklaus
  • Peter Gath
  • Daniel Shaddock

External Research Organisations

  • Max Planck Institute for Gravitational Physics (Albert Einstein Institute)
  • Jet Propulsion Laboratory
  • SpaceTech GmbH Immenstaad (STI)
  • Airbus Group
  • Australian National University
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Details

Original languageEnglish
Title of host publicationInternational Conference on Space Optics, ICSO 2012
EditorsErrico Armandillo, Bruno Cugny, Nikos Karafolas
PublisherSPIE
ISBN (electronic)9781510616172
Publication statusPublished - 20 Nov 2017
Externally publishedYes
EventInternational Conference on Space Optics 2012, ICSO 2012 - Ajaccio, Corsica, France
Duration: 9 Oct 201212 Oct 2012

Publication series

NameProceedings of SPIE - The International Society for Optical Engineering
Volume10564
ISSN (Print)0277-786X
ISSN (electronic)1996-756X

Abstract

The Gravity Recovery and Climate Experiment (GRACE) has produced a wealth of data on Earth gravity, hydrology, glaciology and climate research. To continue that data after the imminent end of the GRACE mission, a follow-on mission is planned to be launched in 2017, as a joint US-German project with a smaller Australian contribution. The satellites will be essentially rebuilt as they were for GRACE using microwave ranging as the primary instrument for measuring changes of the intersatellite distance. In addition and in contrast to the original GRACE mission, a Laser Ranging Interferometer (LRI, previously also called ‘Laser Ranging Instrument’) will be included as a technology demonstrator, which will operate together with the microwave ranging and supply a complimentary set of ranging data with lower noise, and new data on the relative alignment between the spacecraft. The LRI aims for a noise level of 80 nm/ Hz over a distance of up to 270 km and will be the first intersatellite laser ranging interferometer. It shares many technologies with LISA-like gravitational wave observatories. This paper describes the optical architecture including the mechanisms to handle pointing jitter, the main noise sources and their mitigation, and initial laboratory breadboard experiments at AEI Hannover.

ASJC Scopus subject areas

Cite this

Laser Ranging Interferometer for GRACE follow-on. / Heinzel, Gerhard; Sheard, Benjmin; Brause, Nils et al.
International Conference on Space Optics, ICSO 2012. ed. / Errico Armandillo; Bruno Cugny; Nikos Karafolas. SPIE, 2017. 1056420 (Proceedings of SPIE - The International Society for Optical Engineering; Vol. 10564).

Research output: Chapter in book/report/conference proceedingConference contributionResearchpeer review

Heinzel, G, Sheard, B, Brause, N, Danzmann, K, Dehne, M, Gerberding, O, Mahrdt, C, Müller, V, Schütze, D, Stede, G, Klipstein, W, Folkner, W, Spero, R, Nicklaus, K, Gath, P & Shaddock, D 2017, Laser Ranging Interferometer for GRACE follow-on. in E Armandillo, B Cugny & N Karafolas (eds), International Conference on Space Optics, ICSO 2012., 1056420, Proceedings of SPIE - The International Society for Optical Engineering, vol. 10564, SPIE, International Conference on Space Optics 2012, ICSO 2012, Ajaccio, Corsica, France, 9 Oct 2012. https://doi.org/10.1117/12.2309099
Heinzel, G., Sheard, B., Brause, N., Danzmann, K., Dehne, M., Gerberding, O., Mahrdt, C., Müller, V., Schütze, D., Stede, G., Klipstein, W., Folkner, W., Spero, R., Nicklaus, K., Gath, P., & Shaddock, D. (2017). Laser Ranging Interferometer for GRACE follow-on. In E. Armandillo, B. Cugny, & N. Karafolas (Eds.), International Conference on Space Optics, ICSO 2012 Article 1056420 (Proceedings of SPIE - The International Society for Optical Engineering; Vol. 10564). SPIE. https://doi.org/10.1117/12.2309099
Heinzel G, Sheard B, Brause N, Danzmann K, Dehne M, Gerberding O et al. Laser Ranging Interferometer for GRACE follow-on. In Armandillo E, Cugny B, Karafolas N, editors, International Conference on Space Optics, ICSO 2012. SPIE. 2017. 1056420. (Proceedings of SPIE - The International Society for Optical Engineering). doi: 10.1117/12.2309099
Heinzel, Gerhard ; Sheard, Benjmin ; Brause, Nils et al. / Laser Ranging Interferometer for GRACE follow-on. International Conference on Space Optics, ICSO 2012. editor / Errico Armandillo ; Bruno Cugny ; Nikos Karafolas. SPIE, 2017. (Proceedings of SPIE - The International Society for Optical Engineering).
Download
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title = "Laser Ranging Interferometer for GRACE follow-on",
abstract = "The Gravity Recovery and Climate Experiment (GRACE) has produced a wealth of data on Earth gravity, hydrology, glaciology and climate research. To continue that data after the imminent end of the GRACE mission, a follow-on mission is planned to be launched in 2017, as a joint US-German project with a smaller Australian contribution. The satellites will be essentially rebuilt as they were for GRACE using microwave ranging as the primary instrument for measuring changes of the intersatellite distance. In addition and in contrast to the original GRACE mission, a Laser Ranging Interferometer (LRI, previously also called {\textquoteleft}Laser Ranging Instrument{\textquoteright}) will be included as a technology demonstrator, which will operate together with the microwave ranging and supply a complimentary set of ranging data with lower noise, and new data on the relative alignment between the spacecraft. The LRI aims for a noise level of 80 nm/ Hz over a distance of up to 270 km and will be the first intersatellite laser ranging interferometer. It shares many technologies with LISA-like gravitational wave observatories. This paper describes the optical architecture including the mechanisms to handle pointing jitter, the main noise sources and their mitigation, and initial laboratory breadboard experiments at AEI Hannover.",
author = "Gerhard Heinzel and Benjmin Sheard and Nils Brause and Karsten Danzmann and Marina Dehne and Oliver Gerberding and Christoph Mahrdt and Vitali M{\"u}ller and Daniel Sch{\"u}tze and Gunnar Stede and William Klipstein and William Folkner and Robert Spero and Kolja Nicklaus and Peter Gath and Daniel Shaddock",
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AU - Heinzel, Gerhard

AU - Sheard, Benjmin

AU - Brause, Nils

AU - Danzmann, Karsten

AU - Dehne, Marina

AU - Gerberding, Oliver

AU - Mahrdt, Christoph

AU - Müller, Vitali

AU - Schütze, Daniel

AU - Stede, Gunnar

AU - Klipstein, William

AU - Folkner, William

AU - Spero, Robert

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AU - Gath, Peter

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N1 - Funding Information: This work was partly funded by the “Deutsche Forschungs-gemeinschaft” (DFG) within the Cluster of Excellence QUEST (Centre for Quantum Engineering and Space-Time Research). Parts of the research described in this publication were carried out at the Jet Propulsion Laboratory, California Institute of Technology, under a contract with the National Aeronautics and Space Administration. This work was also supported under the Australian Government’s Australian Space Research Program.

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N2 - The Gravity Recovery and Climate Experiment (GRACE) has produced a wealth of data on Earth gravity, hydrology, glaciology and climate research. To continue that data after the imminent end of the GRACE mission, a follow-on mission is planned to be launched in 2017, as a joint US-German project with a smaller Australian contribution. The satellites will be essentially rebuilt as they were for GRACE using microwave ranging as the primary instrument for measuring changes of the intersatellite distance. In addition and in contrast to the original GRACE mission, a Laser Ranging Interferometer (LRI, previously also called ‘Laser Ranging Instrument’) will be included as a technology demonstrator, which will operate together with the microwave ranging and supply a complimentary set of ranging data with lower noise, and new data on the relative alignment between the spacecraft. The LRI aims for a noise level of 80 nm/ Hz over a distance of up to 270 km and will be the first intersatellite laser ranging interferometer. It shares many technologies with LISA-like gravitational wave observatories. This paper describes the optical architecture including the mechanisms to handle pointing jitter, the main noise sources and their mitigation, and initial laboratory breadboard experiments at AEI Hannover.

AB - The Gravity Recovery and Climate Experiment (GRACE) has produced a wealth of data on Earth gravity, hydrology, glaciology and climate research. To continue that data after the imminent end of the GRACE mission, a follow-on mission is planned to be launched in 2017, as a joint US-German project with a smaller Australian contribution. The satellites will be essentially rebuilt as they were for GRACE using microwave ranging as the primary instrument for measuring changes of the intersatellite distance. In addition and in contrast to the original GRACE mission, a Laser Ranging Interferometer (LRI, previously also called ‘Laser Ranging Instrument’) will be included as a technology demonstrator, which will operate together with the microwave ranging and supply a complimentary set of ranging data with lower noise, and new data on the relative alignment between the spacecraft. The LRI aims for a noise level of 80 nm/ Hz over a distance of up to 270 km and will be the first intersatellite laser ranging interferometer. It shares many technologies with LISA-like gravitational wave observatories. This paper describes the optical architecture including the mechanisms to handle pointing jitter, the main noise sources and their mitigation, and initial laboratory breadboard experiments at AEI Hannover.

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