18-20 October 2022
ESA/ESTEC
Europe/Amsterdam timezone

JUICE (JUpiter ICy moon Explorer) thermal model correlation and final flight thermal predictions

20 Oct 2022, 09:30
30m
Newton

Newton

thermal design (for platforms, instruments etc.) Thermal Design

Speakers

Romain PEYROU-LAUGA (ESA) Mr Gabriel ROCA (Airbus Defence and Space)

Description

JUICE - JUpiter ICy moons Explorer - is the first large-class mission in ESA's Cosmic Vision 2015-2025 programme. Planned for launch in 2022 and arrival at Jupiter in 2031, it will spend at least three years making detailed observations of the giant gaseous planet Jupiter and three of its largest moons, Ganymede, Callisto and Europa.
The JUICE spacecraft will carry the most powerful remote sensing, geophysical, and in situ payload complement ever flown to the outer Solar System. The payload consists of 10 state-of-the-art instruments.
JUICE spacecraft thermal control has to cope with a large variation of external environment during the mission (Sun flux from 3323 W/m² in the inner Solar System down to 46 W/m² in Jovian environment) and long eclipses of up to 4.8 hours.
The JUICE thermal control is designed with the objective to minimize the impact of the external environment on the spacecraft through high efficiency Multi-Layer Insulation. Minimizing heating power demand especially during science and communication phases and minimizing hardware mass is a constant concern and solutions are found to build to a maximum extent a robust and passive thermal design supplemented by heaters.
JUICE Spacecraft performed its Thermal Vacuum and Thermal Balance Test in 2021. This presentation will focus on the thermal model correlation after the thermal test and will present the overall final flight thermal predictions.

Primary authors

Romain PEYROU-LAUGA (ESA) Mr Gabriel ROCA (Airbus Defence and Space)

Presentation Materials