JOKARUS - design of a compact optical iodine frequency reference for a sounding rocket mission. Schkolnik, V., Döringshoff, K., Gutsch, F. B., Oswald, M., Schuldt, T., Braxmaier, C., Lezius, M., Holzwarth, R., Kürbis, C., Bawamia, A., Krutzik, M., & Peters, A. EPJ Quantum Technology, 4(1):9, May, 2017. Paper doi abstract bibtex We present the design of a compact absolute optical frequency reference for space applications based on hyperfine transitions in molecular iodine with a targeted fractional frequency instability of better than 3 \texttimes 10−14 after 1 s. It is based on a micro-integrated extended cavity diode laser with integrated optical amplifier, fiber pigtailed second harmonic generation wave-guide modules, and a quasi-monolithic spectroscopy setup with operating electronics. The instrument described here is scheduled for launch end of 2017 aboard the TEXUS 54 sounding rocket as an important qualification step towards space application of iodine frequency references and related technologies. The payload will operate autonomously and its optical frequency will be compared to an optical frequency comb during its space flight.
@Article{Schkolnik2017,
author="Schkolnik, Vladimir
and D{\"o}ringshoff, Klaus
and Gutsch, Franz Balthasar
and Oswald, Markus
and Schuldt, Thilo
and Braxmaier, Claus
and Lezius, Matthias
and Holzwarth, Ronald
and K{\"u}rbis, Christian
and Bawamia, Ahmad
and Krutzik, Markus
and Peters, Achim",
title="JOKARUS - design of a compact optical iodine frequency reference for a sounding rocket mission",
journal="EPJ Quantum Technology",
year="2017",
month="May",
day="22",
volume="4",
number="1",
pages="9",
abstract="We present the design of a compact absolute optical frequency reference for space applications based on hyperfine transitions in molecular iodine with a targeted fractional frequency instability of better than 3 {\texttimes} 10−14 after 1 s. It is based on a micro-integrated extended cavity diode laser with integrated optical amplifier, fiber pigtailed second harmonic generation wave-guide modules, and a quasi-monolithic spectroscopy setup with operating electronics. The instrument described here is scheduled for launch end of 2017 aboard the TEXUS 54 sounding rocket as an important qualification step towards space application of iodine frequency references and related technologies. The payload will operate autonomously and its optical frequency will be compared to an optical frequency comb during its space flight.",
issn="2196-0763",
doi="10.1140/epjqt/s40507-017-0063-y",
url="https://doi.org/10.1140/epjqt/s40507-017-0063-y"
}
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