Presentation #412.06 in the session “Future Instruments, Missions and Facilities”.
Comets are strongly deserving of in situ study as they largely preserve material formed at our Solar System’s birth. In 2019, Comet Interceptor was selected by the European Space Agency, ESA, as the first in its new class of Fast (F) projects [Snodgrass & Jones, Nature Comms. 10, 5418, 2019]. The Japanese space agency, JAXA, is making a major contribution to the project.
The mission’s primary science goal is to characterise for the first time, a yet-to-be-discovered long-period comet, preferably dynamically new, or an interstellar object. An encounter with a comet approaching the Sun for the first time will provide valuable data to complement that from all previous comet missions, which visited more evolved short period comets. The target’s surface temperature could be above its constituent ices’ sublimation points for the first time.
Following a 2029 launch, the spacecraft will be delivered to the Sun-Earth L2 Lagrange Point. This relatively stable location allows a rapid response to the appearance of a suitable target comet, which will need to cross the ecliptic plane in an annulus containing Earth’s orbit. A suitable new comet would be searched for from Earth, with short period comets serving as backup targets. Powerful facilities such as the Vera Rubin Observatory make finding a suitable comet nearing the Sun very promising. The spacecraft could encounter an interstellar object if one is found on a suitable trajectory.
The spacecraft must cope with a wide range of target activity levels, flyby speeds, and encounter geometries. This flexibility has significant impacts on its solar power input, thermal design, and dust shielding that can cope with dust impacts from 10 to 70 km/s, depending on the target comet’s orbit. Comet Interceptor comprises a main spacecraft and two probes, one provided by ESA, the other by JAXA, which will be released by the main spacecraft on approach. The main spacecraft, which would act as the primary communication point for the whole constellation, would be targeted to pass outside the hazardous inner coma, making remote and in situ observations on the comet’s sunward side.
Planned measurements of the target include its surface composition, shape, and structure, its dust environment, and the gas coma’s composition. A unique, multi-point ‘snapshot’ of the comet- solar wind interaction region will be obtained, complementing single spacecraft observations at other comets. We shall describe the science drivers, planned observations, and the mission’s instrument complement, to be provided by consortia of institutions in Europe and Japan.
Team members are listed at www.cometinterceptor.space