The Truths Mission

The Traceable Radiometry Underpinning Terrestrial- and Helio-Studies (Truths), mission will be a ‘standards laboratory in space’, setting the ‘gold standard’ reference for climate measurements. Carrying a cryogenic solar absolute radiometer and a hyperspectral imaging spectrometer as well as a novel onboard calibration system, Truths will make continuous measurements of incoming solar radiation and reflected radiation to evaluate Earth’s energy-in to energy-out ratio.

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Source and credits: ESA, PMOD/WRC

 

PMOD/WRC Instrument: Truths - Cryogenic Solar Absolute Radiometer (CSAR)

Scientific Objectives

The Cryogenic Solar Absolute Radiometer (CSAR) onboard the ESA TRUTHS mission will measure the Total Solar Irradiance with unprecedented accuracy and do in-orbit calibration of the Hyperspectral Imaging Spectrometer, allowing SI-traceable hyperspectral images of the Earth to be taken. The launch is planned for 2030.

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TRUTHS-CSAR Progress to Date

Phase B2 kicked-off at the beginning of 2024, which is dedicated to designing and building a prototype (breadboard) of the instrument to demonstrate the technology in a relevant environment. PMOD/WRC, as part of the Swiss consortium led by Thales Alenia Space Switzerland, designed, manufactured, and assembled the majority of the measurement block as well as the front-end electronics (FEE). The rest of the consortium (Thales Alenia Space Switzerland & Micos Engineering GmbH, Switzerland) was in charge of the breadboard cryostat and the precision apertures with the cover-plate that they are mounted on. Tests on the prototype instrument will be performed in the first quarter of 2025, and will culminate in a Preliminary Design Review (PDR) at the end of the year.

Progress was made at PMOD/WRC in the area of: i) machining thin-walled absorbing black bodies, which are coated with carbon-nanotubes (Figure 1), ii) manufacturing cryogenic temperature sensors out of ultra-thin copper wire (ten meters of wire with a thickness of less than a quarter of a human hair), and iv) SI-traceable electrical power measuring electronics that will be able to fly on a satellite.

Source and credits: ESA, PMOD/WRC

Figure 1. Rear view of a TRUTHS CSAR cavity assembly prototype.

News

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Information

Links

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Main Collaboration Partners

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Swiss Scientific Contact

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Mission Facts

Launch 2030
Launch rocket Vega-C
Orbit Altitude of ~610 km; polar non-Sun-synchronous
Nominal mission duration 5 years
Extended mission duration tbd
PMOD/WRC instrument/involvement TRUTHS – Cryogenic Solar Absolute Radiometer (TRUTHS-CSAR)
Mass
Dimensions
Power consumption
Funding

Source and credits: ESA, PMOD/WRC