Latest Results

JTSIM-DARA Results

Figure 1 shows the minute-rate data recorded by JTSIM-DARA cavities compared with the daily average of the PMO6-v8 product from the VIRGO radiometer onboard SOHO.

First TSI results (Montillet et al., 2023) from the JTSIM-DARAv1 dataset (6-hr frequency at present) can be downloaded here using an FTP client:

ftp://ftp.pmodwrc.ch/pub/data/irradiance/JTSIM/6HourlyRelease/

Montillet, J., Finsterle, W., Koller, S., Pfiffner, D., Gyo, M., (2023), Total Solar Irradiance Recorded by the FY3E/DARA-JTSIM Radiometer, Version 1.0. Interdisciplinary Earth Data Alliance (IEDA), https://doi.org/10.60520/IEDA/113059.

Figure 1. Comparison of Total Solar Irradiance (TSI) from JTSIM-DARA with the VIRGO PMO6V radiometer onboard SOHO. Click on graph to enlarge.

Media and Videos

Media Articles

3. Jul. 2021, Mit China Huckepack in den Orbit, Bündner Zeitung
22. Jun. 2021, Unangenehme Überraschung aus dem Weltall, Davoser Zeitung
30. Jan. 2020, Unerwartet schnell im Weltraum, Südostschweiz Zeitung

Videos

5. Jul. 2021. FY-3E was successfully launched at 23:28 UTC, YouTube

Information

FY-3E Mission

Various space instruments have measured TSI since 1978. One of the latest is the Joint Total Solar Irradiance Monitor (JTSIM) on the Fengyun-3E (FY-3E) satellite. FY-3E is the 5th flight unit of the FY-3 series. Its main mission is operational meteorology. It will provide a substantial contribution to ocean and ice monitoring, climate monitoring, atmospheric chemistry and space weather.  JTSIM has two absolute radiometers on board: the Digital Absolute Radiometer (DARA) developed by PMOD/WRC, and the Solar Irradiance Absolute Radiometer (SIAR), developed by the Changchun Institute of Optics, Fine Mechanics and Physics / Chinese Academy of Sciences (CIOMP/CAS), China. FY-3E was launched on 4 July 2021 at 23:28 UTC according to CASC (China Aerospace Science and Technology Corp.) on a Long March 4C vehicle from the Jiuquan Space Launch Center in China. The orbit is sun-synchronous and near-circular (inclination of 98.7°) with an altitude slightly higher than 800 km. The nominal lifetime of the satellite is eight years. The JTSIM experiment is part of the solar activities monitoring package.

The launch of FY-3E on 4 July 2021. Image credit: ECNS.cn

The measurement of solar irradiance with accuracy sufficiently high to detect and reliably follow small changes (~0.1%) exhibited by the Sun is a remarkable achievement. Measuring the variability of the Sun remains a particular challenge because of the large brightness contrast of the Sun compared to other astronomical objects. Hence, maintaining a photometric calibration using comparisons with stars is difficult.  A high precision and accurate measurement record of the spectrally-integrated total solar irradiance (TSI) arriving at the top of the atmosphere is essential to understand both the energy balance of the Earth’s climate system and the impact of TSI variations on decadal and centennial timescales. TSI is defined as the value of the integrated solar energy flux over the entire spectrum arriving at the top of the terrestrial atmosphere at the mean Sun-Earth distance of 1 AU (the astronomical unit, AU). These measurements are critical inputs to help understand the effects of solar variability on climate.

Source and credits: CIOMP, CMA, PMOD/WRC

PMOD/WRC Instrument: JTSIM-DARA

Scientific Objectives

The JTSIM-DARA/FY-3E instrument is a cooperation with CIOMP (Changchun Institute of Optics, Fine Mechanics and Physics of the Chinese Academy of Sciences), and the China Meteorological Administration (CMA). Key aspects of the FY-3 satellite series include collecting atmospheric data for intermediate and long-term weather forecasting and global climate research. The idea is to operate a standard group of (originally) three electrical substitution radiometers of a different make and model on one satellite, similar to the ground-based World Standard Group (WSG) located at PMOD/WRC, to provide improved long-term stability of TSI measurements. The first realisation of a space standard group will consist of a JTSIM-DARA radiometer, and a SIAR radiometer designed by CIOMP.

Instrument Design and Characteristics

DARA has three electrical substitution cavity radiometers (Channels A, B and C). These are aligned in a triangle. Compared to the VIRGO/PMO6 radiometer, DARA inverts the aperture geometry to eliminate stray-light. The design of the new cavity (and the heat sink system) reduces the so-called non-equivalence effect. The non-equivalence effect is caused by a slightly different thermal configuration of the active cavity in the measurement/calibration phases (i.e. difference in the shutter-closed phases). A different thermal configuration can cause spurious heat flows (e.g. through the surrounding air, or radiation) that are not exactly equal.

The design of the radiometer is based on the early DARA prototype [Suter, 2014] and the Compact Lightweight Absolute Radiometer (CLARA on NorSat-1) [Walter, 2017]. DARA-JTSIM is calibrated and traceable to the World Radiometric Reference of the WSG at PMOD/WRC.The pre-flight calibration and analysis is described in several publications [Song, 2021; Song, 2022a; 2022b; Montillet, 2022].

JTSIM-DARA Results

Figure 1 shows the minute-rate data recorded by JTSIM-DARA cavities compared with the daily average of the PMO6-v8 product from the VIRGO radiometer onboard SOHO.

First TSI results (Montillet et al., 2023a) from the JTSIM-DARAv1 dataset (6-hr frequency at present) can be downloaded here using an FTP client:

ftp://ftp.pmodwrc.ch/pub/data/irradiance/JTSIM/6HourlyRelease/

See also the recently published research paper by Montillet et al. (2023b).

Figure 1. Comparison of Total Solar Irradiance (TSI) from JTSIM-DARA with the VIRGO PMO6V radiometer onboard SOHO. Click on graph to enlarge.

References

Montillet J.-P. et al., (2022), EGU conf. proceedings, https://doi.org/10.5194/egusphere-egu22-616
Montillet, J., Finsterle, W., Koller, S., Pfiffner, D., Gyo, M., (2023a), Total Solar Irradiance Recorded by the FY3E/DARA-JTSIM Radiometer, Version 1.0. Interdisciplinary Earth Data Alliance (IEDA), https://doi.org/10.60520/IEDA/113059
Montillet, J.-P.P., Finsterle, W., Zhu, P., et al., (2023b), Assessment of solar variability through the analysis of TSI observations recorded by the FY3E/JTSIM/DARA radiometer, ESS Open Archive, 27 Dec., https://doi.org/10.22541/essoar.170365223.34450405/v1
Song, B., Ye, X., Finsterle, W. et al., (2021), The Fengyun-3E/Joint Total Solar Irradiance Absolute Radiometer: Instrument Design, Characterization, and Calibration, Sol Phys, 296, 52, https://doi.org/10.1007/s11207-021-01794-5
Song, B., Ye, X., Finsterle, W. et al., (2022a), Correction to: The Fengyun-3E/Joint Total Solar Irradiance Absolute Radiometer: Instrument Design, Characterization, and Calibration, Sol Phys, 297, 111, https://doi.org/10.1007/s11207-022-02056-8
Song, B., Ye, X., Finsterle, W. et al., (2022b), Correction to: The Fengyun-3E/Joint Total Solar Irradiance Absolute Radiometer: Instrument Design, Characterization, and Calibration. Sol Phys, 297, 77, https://doi.org/10.1007/s11207-022-02028-y
Suter, M., (2014), Advances in Solar Radiometry, 2014, University of Zurich, Faculty of Science.
Walter, B. et al., (2017), Metrologia, 54, 67, https://doi.org/10.1088/1681-7575/aa7a63

 

Source and credits: CIOMP, CMA, PMOD/WRC

Mission Facts

Launch date 4 July 2021
Rocket Long March 4C rocket
Orbit Sun-synchronous orbit, altitude 836 km
Nominal mission duration 8 years
PMOD/WRC instrument Joint Total Solar Irradiance Monitor (JTSIM)-DARA radiometer
Mass (satellite) 2300 kg
Mass (JTSIM-DARA) 3.5 kg
Dimensions (satellite)
Dimensions (JTSIM-DARA) 2 units, ~ 1500 cm3 and 2600 cm3
Power consumption (satellite) 2500 W
Power consumption (JTSIM-DARA) 7.4 W
Telemetry (satellite)
Telemetry (JTSIM-DARA)
PMOD/WRC funding ESA PRODEX

 

Source and credits: CIOMP, CMA, PMOD/WRC