Optical Periscopic Imager for Comets (OPIC) Instrument for the Planned Comet Interceptor Mission

This poster presents an update on the development of the Optical Periscopic Imager for Comets (OPIC) instrument [1], which will be hosted on one of three spacecraft making up the Comet Interceptor ESA-JAXA mission [2]. OPIC is a compact ( < 0.5 kg) monochromic camera for taking images of the nucleus and coma of either a long-period or dynamically new comet, or an interstellar object for mapping, reconstruction and localisation purposes. The camera will operate in a harsh environment with continuous dust impacts throughout its multi-day operation; therefore, the instrument is equipped with a periscope, which protects optics from high-velocity impacts. The probe is spin-stabilised at 4-15 RPM and will be parked in Lagrange point L2 (launched with ARIEL telescope) and depart at a suitable time to intercept a target at velocity 10-70 km/s. The closest approach is approximately 400 km.

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Journal
Digital Commons - USU (Utah State University)
Published
2025-08-21
DOI
https://doi.org/10.26077/yh41-7j76
Primary Topic
Astro and Planetary Science
Type
article
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article

Optical Periscopic Imager for Comets (OPIC) Instrument for the Planned Comet Interceptor Mission

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Digital Commons - USU (Utah State University)
Astro and Planetary Science
article

Optical Periscopic Imager for Comets (OPIC) Instrument for the Planned Comet Interceptor Mission

Mihkel Pajusalu, Artiom Nikolajev, Andris Slavinskis, Ullas Bhat, Hans Teras, Iaroslav Iakubivskyi, Joosep Kivastik, Aritra Paul
article en

Abstract

This poster presents an update on the development of the Optical Periscopic Imager for Comets (OPIC) instrument [1], which will be hosted on one of three spacecraft making up the Comet Interceptor ESA-JAXA mission [2]. OPIC is a compact ( < 0.5 kg) monochromic camera for taking images of the nucleus and coma of either a long-period or dynamically new comet, or an interstellar object for mapping, reconstruction and localisation purposes. The camera will operate in a harsh environment with continuous dust impacts throughout its multi-day operation; therefore, the instrument is equipped with a periscope, which protects optics from high-velocity impacts. The probe is spin-stabilised at 4-15 RPM and will be parked in Lagrange point L2 (launched with ARIEL telescope) and depart at a suitable time to intercept a target at velocity 10-70 km/s. The closest approach is approximately 400 km.

Digital Commons - USU (Utah State University)
Tartu Observatory (EE)
Astro and Planetary Science
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