Flight demonstration of a miniature atomic scalar magnetometer based on a microfabricated rubidium vapor cell

• Published in: Review of Scientific Instruments
• Main Authors: Korth, Haje, Kitching, John E., Bonnell, John W., Bryce, Brian A., Clark, George B., Edens, Weston K., Gardner, Christopher B., Rachelson, William, Slagle, Amanda
• Other Authors: NASA Headquarters
• Format: Article in Journal/Newspaper
• Language: English
• Published: AIP Publishing 2023
• Subjects: Instrumentation; Andøya; Norway
• Online Access: http://dx.doi.org/10.1063/5.0135372; https://pubs.aip.org/aip/rsi/article-pdf/doi/10.1063/5.0135372/16798194/035002_1_online.pdf

We have developed an atomic magnetometer based on the rubidium isotope 87Rb and a microfabricated silicon/glass vapor cell for the purpose of qualifying the instrument for space flight during a ride-along opportunity on a sounding rocket. The instrument consists of two scalar magnetic field sensors mounted at 45° angle to avoid measurement dead zones, and the electronics consist of a low-voltage power supply, an analog interface, and a digital controller. The instrument was launched into the Earth’s northern cusp from Andøya, Norway on December 8, 2018 on the low-flying rocket of the dual-rocket Twin Rockets to Investigate Cusp Electrodynamics 2 mission. The magnetometer was operated without interruption during the science phase of the mission, and the acquired data were compared favorably with those from the science magnetometer and the model of the International Geophysical Reference Field to within an approximate fixed offset of about 550 nT. Residuals with respect to these data sources are plausibly attributed to offsets resulting from rocket contamination fields and electronic phase shifts. These offsets can be readily mitigated and/or calibrated for a future flight experiment so that the demonstration of this absolute-measuring magnetometer was entirely successful from the perspective of increasing the technological readiness for space flight.