First in situ measurements of the prototype Tesseract fluxgate magnetometer on the ACES-II-Low sounding rocket

Ongoing innovation in next-generation fluxgate magnetometry is important for enabling future investigations of space plasma, especially multi-spacecraft experimental studies of energy transport in the magnetosphere and the solar wind. Demonstrating the spaceflight capability of novel designs is an i...

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Published in:Geoscientific Instrumentation, Methods and Data Systems
Main Authors: Greene, Kenton, Bounds, Scott R., Broadfoot, Robert M., Feltman, Connor, Hisel, Samuel J., Kraus, Ryan M., Lasko, Amanda, Washington, Antonio, Miles, David M.
Format: Text
Language:English
Published: 2024
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Online Access:https://doi.org/10.5194/gi-13-249-2024
https://gi.copernicus.org/articles/13/249/2024/
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spelling ftcopernicus:oai:publications.copernicus.org:gi117662 2024-09-15T17:39:24+00:00 First in situ measurements of the prototype Tesseract fluxgate magnetometer on the ACES-II-Low sounding rocket Greene, Kenton Bounds, Scott R. Broadfoot, Robert M. Feltman, Connor Hisel, Samuel J. Kraus, Ryan M. Lasko, Amanda Washington, Antonio Miles, David M. 2024-08-01 application/pdf https://doi.org/10.5194/gi-13-249-2024 https://gi.copernicus.org/articles/13/249/2024/ eng eng doi:10.5194/gi-13-249-2024 https://gi.copernicus.org/articles/13/249/2024/ eISSN: 2193-0864 Text 2024 ftcopernicus https://doi.org/10.5194/gi-13-249-2024 2024-08-05T14:04:48Z Ongoing innovation in next-generation fluxgate magnetometry is important for enabling future investigations of space plasma, especially multi-spacecraft experimental studies of energy transport in the magnetosphere and the solar wind. Demonstrating the spaceflight capability of novel designs is an important step in the instrument development process; however, large-scale satellite missions are often unwilling to accept the risks of an instrument without flight heritage. The Tesseract – a novel fluxgate magnetometer sensor design – had an opportunity for an inaugural spaceflight demonstration on the ACES-II sounding rocket mission, which launched from Andøya Space Center in Andenes, Norway, in November 2022. Tesseract's design takes advantage of a new racetrack core geometry to create a sensor that addresses some of the issues that contribute to instability in more traditional ring-core designs. Here we present the design of a prototype fluxgate magnetometer based on the new Tesseract sensor, its pre-flight characteristics, and an evaluation of its in-flight performance aboard ACES-II. We find that the magnetic field measured by Tesseract over the course of the flight was in strong agreement with both the onboard ACES II reference ring-core fluxgate magnetometer and the predictions of a geomagnetic field model. The Tesseract-based magnetometer measured signatures of field-aligned currents and potential Alfvén wave activity as it crossed an active auroral arc, and we conclude that it performed as expected. Tesseract will be flown on the Tandem Reconnection and Cusp Electrodynamics Reconnaissance Satellites (TRACERS) Small Explorers (SMEX) satellite mission as part of the MAGnetometers for Innovation and Capability (MAGIC) technology demonstration currently scheduled to launch in 2025. Text Andenes Andøya Copernicus Publications: E-Journals Geoscientific Instrumentation, Methods and Data Systems 13 2 249 262
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collection Copernicus Publications: E-Journals
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language English
description Ongoing innovation in next-generation fluxgate magnetometry is important for enabling future investigations of space plasma, especially multi-spacecraft experimental studies of energy transport in the magnetosphere and the solar wind. Demonstrating the spaceflight capability of novel designs is an important step in the instrument development process; however, large-scale satellite missions are often unwilling to accept the risks of an instrument without flight heritage. The Tesseract – a novel fluxgate magnetometer sensor design – had an opportunity for an inaugural spaceflight demonstration on the ACES-II sounding rocket mission, which launched from Andøya Space Center in Andenes, Norway, in November 2022. Tesseract's design takes advantage of a new racetrack core geometry to create a sensor that addresses some of the issues that contribute to instability in more traditional ring-core designs. Here we present the design of a prototype fluxgate magnetometer based on the new Tesseract sensor, its pre-flight characteristics, and an evaluation of its in-flight performance aboard ACES-II. We find that the magnetic field measured by Tesseract over the course of the flight was in strong agreement with both the onboard ACES II reference ring-core fluxgate magnetometer and the predictions of a geomagnetic field model. The Tesseract-based magnetometer measured signatures of field-aligned currents and potential Alfvén wave activity as it crossed an active auroral arc, and we conclude that it performed as expected. Tesseract will be flown on the Tandem Reconnection and Cusp Electrodynamics Reconnaissance Satellites (TRACERS) Small Explorers (SMEX) satellite mission as part of the MAGnetometers for Innovation and Capability (MAGIC) technology demonstration currently scheduled to launch in 2025.
format Text
author Greene, Kenton
Bounds, Scott R.
Broadfoot, Robert M.
Feltman, Connor
Hisel, Samuel J.
Kraus, Ryan M.
Lasko, Amanda
Washington, Antonio
Miles, David M.
spellingShingle Greene, Kenton
Bounds, Scott R.
Broadfoot, Robert M.
Feltman, Connor
Hisel, Samuel J.
Kraus, Ryan M.
Lasko, Amanda
Washington, Antonio
Miles, David M.
First in situ measurements of the prototype Tesseract fluxgate magnetometer on the ACES-II-Low sounding rocket
author_facet Greene, Kenton
Bounds, Scott R.
Broadfoot, Robert M.
Feltman, Connor
Hisel, Samuel J.
Kraus, Ryan M.
Lasko, Amanda
Washington, Antonio
Miles, David M.
author_sort Greene, Kenton
title First in situ measurements of the prototype Tesseract fluxgate magnetometer on the ACES-II-Low sounding rocket
title_short First in situ measurements of the prototype Tesseract fluxgate magnetometer on the ACES-II-Low sounding rocket
title_full First in situ measurements of the prototype Tesseract fluxgate magnetometer on the ACES-II-Low sounding rocket
title_fullStr First in situ measurements of the prototype Tesseract fluxgate magnetometer on the ACES-II-Low sounding rocket
title_full_unstemmed First in situ measurements of the prototype Tesseract fluxgate magnetometer on the ACES-II-Low sounding rocket
title_sort first in situ measurements of the prototype tesseract fluxgate magnetometer on the aces-ii-low sounding rocket
publishDate 2024
url https://doi.org/10.5194/gi-13-249-2024
https://gi.copernicus.org/articles/13/249/2024/
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genre_facet Andenes
Andøya
op_source eISSN: 2193-0864
op_relation doi:10.5194/gi-13-249-2024
https://gi.copernicus.org/articles/13/249/2024/
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container_title Geoscientific Instrumentation, Methods and Data Systems
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