News

Can’t stop won’t stop: Solar Orbiter shows the Sun raging on

The hyperactive sunspot region responsible for the beautiful auroras earlier in May was still alive and kicking when it rotated away . . .
ESA, 18 Jun. 2024

Sun’s surprising activity surge in Solar Orbiter snapshot

See how the Sun changed between February 2021 and October 2023. As the Sun approaches the maximum in its magnetic activity cycle, we see more brilliant explosions, dark sunspots . . .
ESA, 13 Feb. 2024

Camera ‘hack’ lets Solar Orbiter peer deeper into Sun’s atmosphere

Scientists have used the ESA/NASA Solar Orbiter’s Extreme Ultraviolet Imager (EUI) in a new mode of operation to record part of the Sun’s atmosphere that . . .
ESA, 6 Sep. 2023

Solar Orbiter discovers tiny jets that could power the solar wind

The ESA/NASA Solar Orbiter spacecraft has discovered a multitude of tiny jets of material escaping from the Sun’s outer atmosphere.
ESA, 24 Aug. 2023

Zooming into the Sun with Solar Orbiter

Solar Orbiter’s latest images shows the full Sun in unprecedented detail. They were taken on 7 March, when the spacecraft was crossing directly between the Earth and Sun . . .
ESA, 24 Mar. 2022

Where is Solar Orbiter at the moment?

View the current position with an ESA interactive 3D-visualisation tool

Media and Videos

Media Articles

16 Jul. 2020. The Sun has never been photographed so close . . . read further in German . . . Tages Anzeiger
17 Jul. 2020. The first pictures have arrived . . . read further in German . . . Davoser Zeitung

TV/Videos

16 Jul. 2020. The first pictures from the Solar Orbiter satellite . . . SRF Swiss Television

Information

Solar Orbiter Mission – The Davos PMOD/WRC is flying to the Sun

What is Solar Orbiter and what is the purpose of this space mission?

Solar Orbiter is a 2.5 x 3.1 x 2.7 m and 1800 kg spacecraft from the European Space Agency (ESA). It will orbit the Sun at a similar distance to Mercury, the closest of all planets to the Sun. The aim of the Solar Orbiter mission is to investigate the regularly occurring solar flares in the form of huge plasma bubbles. The previously unknown polar regions of the sun are a particular focus. Ten instruments are onboard the spacecraft. They make it possible to look at the sun using telescopes and cameras and to relay images of the solar poles for the first time in the history of space research.

What is the point of the mission?

The eruptions emanating from the sun are responsible for so-called space weather. This is noticeable here on Earth, for example in the form of the polar auorae. However, space weather can sometimes have negative consequences: solar storms caused by violent solar flares can disrupt GPS, but also other technologies and electrical systems on which our civilization depends more and more. If space weather can be predicted more precisely, such failures can be avoided in the future. Solar Orbiter will investigate the scientific connections behind space weather and thus help to improve the space weather forecast.

How and when will Solar Orbiter go into space?

It takes a rocket (Atlas V) to launch Solar Orbiter into space. If everything goes according to plan, the spacecraft will launch from Cape Canaveral (Florida) on 10 February at 05:03 CET at a speed of 58,000 km/h – around 60 times faster than the average passenger plane. As every detail has to be right for such a start, the exact start time can be postponed for hours, if not days.

Who is involved in the mission and how long will it last?

The idea for Solar Orbiter came up in 1996. Since then, scientists and companies from 18 countries have been working on the mission. The measuring instruments will provide the first data around three to four months after the start. It takes around a year and a half for Solar Orbiter to reach tis definitive orbit. It is planned that the Solar Orbiter will transmit data from space for around seven years.

How is the PMOD/WRC involved in Solar Orbiter?

The PMOD/WRC in Davos was involved in the design and construction of two instruments, EUI (Extreme Ultraviolet Imager) and SPICE (Spectral Imaging of the Coronal Environment). EUI consists of three telescopes with extreme ultraviolet cameras. One of the telescopes takes in the whole sun, the other two provide high-resolution images of fine structures. SPICE also captures a specific area of the sun, but at different wavelengths.

Apart from PMOD/WRC, are there any other Swiss partners who are working on  auch noch weitere Partner aus der Schweiz, die an Solar Orbiter mitarbeiten?

The Fachholschule Nordwestschweiz (FHNW) has developed an X-ray telescope that will also be on board Solar Orbiter. Almatec and RUAG, two industrial partners from Switzerland, were also involved in the construction of the instrument.

What are the greatest challenges for Solar Orbiter?

It will be VERY hot where Solar Orbiter orbits! At its closest point to the sun, the front of the spacecraft will reach 500°C. The average smartphone stops working at temperatures between 35 and 45°C! A huge heat-shield (3.2 x 2.4 m) therefore protects the instruments made from very sensitive electronics and optics. The heat-shield is constructed of titanium (used for instance in joint prosthetics developed by the AO Foundation Davos), and a special material called SolarBlack, which is obtained from burned animal bones. So that the instruments can take pictures of the sun despite this heat protection, small recesses with doors are built into the shield, which will opened at the appropriate time.

In addition to the risk of burning the measuring instruments, there are many things that could also go wrong during the mission, from a possible explosion of the spacecraft at launch to missing the intended orbit or jamming of heat-shield doors.

What skills and professions are required for a space mission such as Solar Orbiter?

Scientists develop international instruments to uncover the secrets of the sun. A traditional academic path through university is usually required, specialising in physics or mathematics, and obtaining a doctorate.

Electronic Engineers design complex electronics that capture, process and transmit the data collected from all instruments on board. Entry into this field can be via an apprenticeship in electronics with a subsequent university of applied sciences or university degree, e.g. in electronics or physics.

Mechanical Engineers are responsible for designs that withstand the shocks during takeoff and hold the instruments in precise positions throughout the mission. Entry into this field can be via an apprenticeship with a subsequent university of applied sciences or university degree in mechanical engineering.

Optical Engineers design telescopes that are compact enough to fit on a spacecraft and can directly observe the sun without going “blind”. Entry into this field can be via training or research in physics.

Software Engineers develop software that can automatically run reliably millions of miles from Earth in a harsh radiation environment. Different training paths are possible – usually with a mathematical, computer science, physical or engineering background.

Project Managers ensure that all of the above do their work on time and on budget and that all parts of the system work well together. They can have any professional background – from technical to military.

Source and credits: ESA, NASA, PMOD/WRC

Science Overview

Solar Orbiter is a mission dedicated to solar and heliospheric physics. It was selected as the first medium-class mission of ESA’s Cosmic Vision 2015 – 2025 Programme. The programme outlines key scientific questions which need to be answered about the development of planets and the emergence of life, how the Solar System works, the origins of the Universe, and the fundamental physics at work in the Universe.

Solar Orbiter is specially designed to always point to the Sun, and so, its Sun-facing side is protected by a sunshield. The spacecraft will also be kept cool by the positioning of special radiators, which will dissipate excess heat into space. The solar arrays and the communications system are inherited from the design of ESA’s BepiColombo mission to Mercury.

Solar Orbiter will carry a number of highly sophisticated, lightweight instruments, weighing a total of 180 kg. One suite consists of detectors meant to observe particles and events in the immediate vicinity of the spacecraft. These include the charged particles and magnetic fields of the solar wind, radio and magnetic waves in the solar wind, and energetic charged particles.

The other set of instruments will observe the Sun’s surface and atmosphere. The gas of the atmosphere is best seen by its strong emission of short-wavelength ultraviolet rays. Tuned to these will be a full-Sun and high-resolution imager and a high-resolution spectrometer. The outer atmosphere will be revealed by visible-light and ultraviolet coronagraphs that blot out the bright disc of the Sun. To examine the surface by visible light, and measure local magnetic fields, Solar Orbiter will carry a high-resolution magnetograph.

The suite of in-situ and remote-sensing instruments will significantly contribute to the following Solar Orbiter scientific themes:

  • What drives the solar wind and where does the coronal magnetic field originate from?
  • How do solar transients drive heliospheric variability?
  • How do solar eruptions produce energetic particle radiation that fills the heliosphere?
  • How does the solar dynamo work and drive connections between the Sun and the heliosphere?

In-Situ Instruments

EPD: Energetic Particle Detector
Principal Invest.: Javier Rodríguez-Pacheco, Univ. Alcalá, Spain
Collaborating countries (hardware): Spain, Germany, USA, ESA
EPD will measure the composition, timing and distribution functions of suprathermal and energetic particles. Scientific topics to be addressed include the sources, acceleration mechanisms, and transport processes of these particles.

MAG: Magnetometer
Principal Investigator: Timothy Horbury, Imp. College London, UK
Collaborating countries (hardware): UK
The magnetometer will provide in situ measurements of the heliospheric magnetic field with high precision. This will facilitate detailed studies into the way the Sun’s magnetic field links into space and evolves over the solar cycle; how particles are accelerated and propagate around the Solar System, including to the Earth; how the corona and solar wind are heated and accelerated.

Figure 1. Cross-section of Solar Orbiter showing the configuration of the 10 in-situ and remote-sensing scientific instruments.

RPW: Radio and Plasma Waves
Principal Investigator: Milan Maksimovic, LESIA, Observatoire de Paris, Meudon, France
Collaborating Countries (hardware): France, Sweden, Czech Republic, Austria

The RPW experiment is unique amongst the Solar Orbiter instruments in that it makes both in situ and remote-sensing measurements. RPW will measure magnetic and electric fields at high time resolution using a number of sensors/antennas, to determine the characteristics of electromagnetic and electrostatic waves in the solar wind.

SWA: Solar Wind Plasma Analyser
Principal Investigator: Christopher J. Owen, Mullard Space Science Laboratory, United Kingdom
Collaborating countries (hardware): United Kingdom, Italy, France, USA

The Solar Wind Plasma Analyser, SWA, consists of a suite of sensors that will measure the ion and electron bulk properties (including, density, velocity, and temperature) of the solar wind, thereby characterising the solar wind between 0.28 and 1.4 AU from the Sun. In addition to determining the bulk properties of the wind, SWA will provide measurements of solar wind ion composition for key elements (e.g. the C, N, O group and Fe, Si or Mg).

 

Remote-Sensing Instruments

EUI: Extreme Ultraviolet Imager
Principal Investigator: David Berghmans, Royal Observatory of Belgium, Brussels, Belgium
Collaborating countries (hardware): Belgium, United Kingdom, France, Germany, Switzerland

EUI will provide image sequences of the solar atmospheric layers above the photosphere, thereby providing an indispensable link between the solar surface and outer corona that ultimately shapes the characteristics of the interplanetary medium. EUI will also provide the first-ever UV images of the Sun from an out-of-ecliptic viewpoint (up to 34° of solar latitude during the extended mission phase).

METIS: Coronagraph
Principal Investigator: Marco Romoli, INAF – University of Florence, Italy
Collaborating countries (hardware): Italy, Germany, Czech Republic
METIS will simultaneously image the visible, ultraviolet and extreme ultraviolet emission of the solar corona and diagnose, with unprecedented temporal coverage and spatial resolution, the structure and dynamics of the full corona in the range from 1.4 to 3.0 (from 1.7 to 4.1) solar radii from Sun centre, at minimum (maximum) perihelion during the nominal mission. This is a region that is crucial in linking the solar atmospheric phenomena to their evolution in the inner heliosphere.

PHI: Polarimetric and Helioseismic Imager
Principal Investigator: Sami Solanki, Max-Planck-Institut für Sonnensystemforschung, Göttingen, Germany
Collaborating countries (hardware): Germany, Spain, France
The Polarimetric and Helioseismic Imager, PHI, will provide high-resolution and full-disc measurements of the photospheric vector magnetic field and line-of-sight (LOS) velocity as well as the continuum intensity in the visible wavelength range. The LOS velocity maps will have the accuracy and stability to allow detailed helioseismic investigations of the solar interior, in particular of the solar convection zone.

SoloHI: Heliospheric Imager
Principal Investigator: Russell A. Howard, US Naval Research Laboratory, Washington, D.C., USA
Collaborating countries (hardware): USA
This instrument will image both the quasi-steady flow and transient disturbances in the solar wind over a wide field of view by observing visible sunlight scattered by solar wind electrons. It will provide unique measurements to pinpoint coronal mass ejections (CMEs).

SPICE: Spectral Imaging of the Coronal Environment
Principal Investigator: Not applicable – European-led facility instrument
Principal Investigator for Operations Phase: Frédéric Auchère, Institut d’Astrophysique Spatiale, Orsay, France
Collaborating countries (hardware): United Kingdom, Germany, France, Switzerland, USA
This instrument will perform extreme ultraviolet imaging spectroscopy to remotely characterize plasma properties of the Sun’s on-disc corona. This will enable matching in-situ composition signatures of solar wind streams to their source regions on the Sun’s surface.

STIX: X-ray Spectrometer/Telescope
Principal Investigator: Samuel Krucker, FHNW, Windisch, Switzerland
Collaborating countries (hardware): Switzerland, Poland, Germany, Czech Republic, France
STIX provides imaging spectroscopy of solar thermal and non-thermal X-ray emission. STIX will provide quantitative information on the timing, location, intensity, and spectra of accelerated electrons as well as of high temperature thermal plasmas, mostly associated with flares and/or microflares.

Source and credits: ESA, NASA, PMOD/WRC

PMOD/WRC Involvement: The EUI and SPICE Instruments

PMOD/WRC was involved in the construction of the EUI (Fig. 1) and SPICE (Figs. 2-4) instruments on board Solar Orbiter. The EUI Optical Bench Structure was built by APCO Technologies and PMOD/WRC. The SPICE low-voltage power supply was built at PMOD/WRC. In addition, the SPICE Slit Change Mechanism was constructed by Almatech, and the SPICE Contamination Door by APCO Technologies, both managed by PMOD/WRC.

Scientific Objectives

EUI will provide image sequences of the solar atmospheric layers above the photosphere, thereby providing an indispensable link between the solar surface and outer corona that ultimately shapes the characteristics of the interplanetary medium. EUI will also provide the first-ever UV images of the Sun from an out-of-ecliptic viewpoint (up to 34° of solar latitude during the extended mission phase).

EUI has an instrument suite composed of a Full Sun Imager (FSI) and two High Resolution Imagers (HRI). HRI and FSI have spatial resolutions of 1 and 9 arc seconds, respectively. The HRI cadence depends on the target and can reach sub-second values to observe the fast dynamics of small-scale features. The FSI cadence will be ~10 minutes in each passband, but can also achieve low cadences of ~10 s. The FSI works alternately in two passbands, 174 Å and 304 Å, while the two HRI passbands observe in the hydrogen Lyman a (1216 Å) and the extreme UV (174 Å).

SPICE is a high resolution imaging spectrometer operating at extreme ultraviolet (EUV) wavelengths, 70.4 – 79.0 nm and 97.3 – 104.9 nm. SPICE will perform extreme ultraviolet imaging spectroscopy to remotely characterise plasma properties of the Sun’s on-disc corona. This will enable matching in-situ composition signatures of solar wind streams to their source regions on the Sun’s surface.

The EUV wavelength region observed by SPICE is dominated by emission lines from a wide range of ions formed in the solar atmosphere at temperatures from 10000 to 10 Million Kelvin. SPICE will measure plasma densities and temperatures, flow velocities, the presence of plasma turbulence and the composition of the source region plasma. It will observe the energetics, dynamics and fine-scale structure of the Sun’s magnetised atmosphere at all latitudes.

Figure 1. EUI flight model.

Figure 2. SPICE door mechanism.

Figure 3. SPICE low voltage power supply.

Figure 4. SPICE flight model.

Mission Facts

Launch 05:03 CET 10 Feb. 2020 (Cape Canaveral, USA)
Launch rocket Atlas V
Orbit Perihelion distance to the Sun: 42 x 106 km
Nominal mission duration

Commissioning phase: until 15 Jun. 2020

Cruise phase: 15 Jun. 2020 – Nov. 2021

Science phase: Nov. 2021 – +4 years

Extended mission duration up to 3 years
PMOD/WRC instruments/involvement SPICE and EUI instruments
Instrument payload mass 209 kg
Dimensions (satellite) 2.5 x 3.5 x 2.7 m
Payload power 180 W
Funding  Swiss Space Office SSO / ESA PRODEX Programme

 

ESA Fact Sheets

Solar Orbiter Fact Sheet No. 1
Solar Orbiter Fact Sheet No. 2

Source and credits: ESA, NASA, PMOD/WRC