The Traceable Radiometry Underpinning Terrestrial- and Helio-Studies mission (TRUTHS) is a planned European Space Agency (ESA) satellite. It is meant to "improve the accuracy, reliability and integrity" of Earth observation (EO) data,[2] and to be the first of a new class of "SI-traceable satellites" (SITSats) that will enable other EO missions to calibrate measurements with reference to them.[3]

Quick Facts Names, Mission type ...
TRUTHS
NamesTraceable Radiometry Underpinning Terrestrial- and Helio-Studies
Mission typeSolar radiation measurement, traceability
Mission duration5-8+ years (planned)
Start of mission
Launch date~2030
RocketVega-C (planned)
Launch siteCentre Spatial Guyanais
Orbital parameters
Reference systemGeocentric
RegimePolar
Altitude610 km
Inclination90°
Period96.9 minutes[1]
Repeat interval61 days
Instruments
CSAR - cryogenic solar absolute radiometer
HIS - hyperspectral imaging spectrometer
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Science

Alongside communications and navigation equipment, the scientific payload of the satellite would include three instruments: the cryogenic solar absolute radiometer (CSAR), the onboard calibration system (OBCS), and the hyperspectral imaging spectrometer (HIS). The instruments would produce global hyperspectral (320 nm to 2400 nm) measurements of "top-of-atmosphere earth spectral radiance (0.3% k=2); solar irradiance (both total and spectrally resolved, 0.02% and 0.3% respectively); and lunar spectral irradiance (0.3%)".[3]

The cryogenic radiometer is the primary standard used by national metrology institutes for radiometric measurements and "recommended as the means to achieve SI traceability".[4] The CSAR, which would be cooled to <60 K, is therefore considered "the heart of the calibration system".[4] The mission would be the first to host a primary standard cryogenic radiometer aboard a satellite.[3] The OBCS would "....transfer calibration traceability from the SI defining power measurement...to a full spectrally resolved radiance calibration of an instrument" – in the case of TRUTHS from the CSAR to the HIS – in a simplified manner to the steps used by terrestrial metrology institutes.[4] The HIS can then be used to image the Earth, the Moon, and also to "measure incident solar spectral irradiance."[4]

The mission is led by the UK National Physical Laboratory (NPL) and its lead scientist for EO, Nigel Fox.[5] It has two primary objectives:[6]

"Climate benchmarking through high-accuracy direct hyperspectral measurements of the Earth’s incoming and outgoing radiation to enhance our ability to estimate the Earth’s radiation budget by an order of magnitude, enabling detection of climate signals in the shortest possible time."

"To establish a "gold-standard" reference dataset against which to cross-calibrate other sensors, facilitating an upgrade to the performance of the global Earth observing system to ensure interoperability and robust anchoring to an SI reference in space."

A secondary objective of the mission is the use the global hyperspectral data to "constrain and improve retrieval algorithms".[4]

Development

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TRUTHS mission patch
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In order to obtain both scientific and financial support for the mission, many reports and academic publications were produced by Fox and collaborators over several decades.[9][10][11][12][13][14]

Timeline:[15]

  • Early 2000s – Mission proposed by the UK National Physical Laboratory (NPL)
  • 2019 – Adopted at the ESA ministerial conference, with 85% funding from the UK. The remainder from Switzerland, Greece, Czechia, and Romania.[16][17]
  • 2020 – Airbus UK selected as lead contractor,[18] Teledyne e2v selected to provide the infrared detectors.[19]
  • 2021 – At COP26: Began early design phase.[20]
  • 2022 – Passed preliminary design, technical, and scientific reviews.[21] Received further funding at the ESA ministerial conference.[22]
  • 2023 – Further funding awarded during COP28, to Airbus UK for design and development; and to Teledyne e2v to construct the hyperspectral imaging spectrometer detection system.[23]
  • ~ 2030 – Estimated launch, aboard a Vega-C from the Guiana Space Centre.

The mission would have a targeted duration of eight or more years, and a minimum duration of five.[4]

See also

References

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