| TRUTHS mission patch | |
| Names | Traceable Radiometry Underpinning Terrestrial- and Helio-Studies |
|---|---|
| Mission type | Solar radiation measurement, traceability |
| Mission duration | 5-8+ years (planned) |
| Start of mission | |
| Launch date | ~2030 |
| Rocket | Vega-C (planned) |
| Launch site | Centre Spatial Guyanais |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Polar |
| Altitude | 610 km |
| Inclination | 90° |
| Period | 96.9 minutes [1] |
| Repeat interval | 61 days |
| Instruments | |
| CSAR - cryogenic solar absolute radiometer HIS - hyperspectral imaging spectrometer | |
TRUTHS(Traceable Radiometry Underpinning Terrestrial- and Helio-Studies) is a planned European Space Agency (ESA) satellite. It is meant to improve the accuracy, reliability, and integrity of Earth observation data, [2] and to be the first of a new class of "SI-traceable satellites" (SITSats) that will enable other Earth observation missions to calibrate measurements with reference to them. [3] The mission is led by the UK National Physical Laboratory (NPL) and its lead scientist for Earth observation, Nigel Fox. [4]
It has two primary objectives: [5]
A secondary objective of the mission is the use the global hyperspectral data to "constrain and improve retrieval algorithms". [6]
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". [6] The CSAR, which would be cooled to < 60 K, is therefore considered "the heart of the calibration system". [6]
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. [6] The HIS can then be used to image the Earth, the Moon, and also to "measure incident solar spectral irradiance." [6]
| External videos | |
|---|---|
| | |
| |