This article needs to be updated.March 2020)(
Artist's impression of the Solar Orbiter.
|Mission type||Solar heliophysics orbiter|
|Operator||ESA / NASA|
|Mission duration||7 years (nominal)|
+ 3 years (extended)
|Manufacturer||Airbus Defence and Space|
|Launch mass||1,800 kg (4,000 lb)|
|Payload mass||209 kg (461 lb)|
|Dimensions||2.5 x 3.0 x 2.5 m|
|Start of mission|
|Launch date||10 February 2020, 04:03 UTC|
|Rocket||Atlas V 411 (AV-087)|
|Launch site||Cape Canaveral, SLC-41|
|Contractor||United Launch Alliance|
|Entered service||November 2021|
(start of main mission)
|Perihelion altitude||0.28 au|
|Aphelion altitude||0.91 au|
|Inclination||25° (nominal mission)|
33° (extended mission)
|Focal length||2.5 m|
|Wavelengths||Visible light, ultraviolet, X-rays|
Insignia for the Solar Orbiter mission.
The Solar Orbiter (SolO) is a Sun-observing satellite, developed by the European Space Agency (ESA). SolO is intended to perform detailed measurements of the inner heliosphere and nascent solar wind, and perform close observations of the polar regions of the Sun, which is difficult to do from Earth, both serving to answer the question "How does the Sun create and control the heliosphere?"
SolO will make observations of the Sun from an eccentric orbit moving as close as ~60 solar radii (RS), or 0.284 astronomical units (au), placing it inside Mercury's perihelion of 0.3075 au. During the mission the orbital inclination will be raised to about 25°. The total mission cost is US$1.5 billion, counting both ESA and NASA contributions.
SolO was launched on 10 February 2020. The mission is planned to last 7 years.
The Solar Orbiter spacecraft is a Sun-pointed, three-axis stabilised platform with a dedicated heat shield to provide protection from the high levels of solar flux near perihelion. The spacecraft provides a stable platform to accommodate the combination of remote-sensing and in situ instrumentation in an electromagnetically clean environment. The 21 sensors were configured on the spacecraft to allow each to conduct its in situ or remote sensing experiments with both access to and protection from the solar environment. Solar Orbiter has inherited technology from previous missions, such as the solar arrays from the BepiColombo Mercury Planetary Orbiter (MPO). The solar arrays can be rotated about their longitudinal axis to avoid overheating when close to the Sun. A battery pack provides supplementary power at other points in the mission such as eclipse periods encountered during planetary flybys.
The Telemetry, Tracking and Command Subsystem provides the communication link capability with the Earth in X-band. The subsystem supports telemetry, telecommand and ranging. Low-Gain Antennas are used for Launch and Early Orbit Phase (LEOP) and will also be available as a back-up during the mission phase when steerable Medium- and High-Gain Antennas will be in use. The High-Temperature High-Gain Antenna needs to point to a wide range of positions to achieve a link with the ground station and to be able to downlink sufficient volumes of data. Its design was adapted from the BepiColombo mission. The antenna can be folded in to gain protection from Solar Orbiter's heat shield if necessary. Most data will therefore initially be stored in on-board memory and sent back to Earth at the earliest possible opportunity.
The ground station at Malargüe (Argentina), with a 35-m antenna, for 4 to 8 hours/day (effective). ESA's Malargüe ground station will be used for all operations throughout the mission with the ground stations in New Norcia, Australia, and Cebreros, Spain, acting as backup when necessary.
During nominal science operations, science data will be downlinked for eight hours during each communication period with the ground station. Additional eight-hour downlink passes will be scheduled as needed to reach the required total science data return of the mission. The Solar Orbiter ground segment will make maximum reuse of ESA's infrastructure for Deep Space missions:
- The ground stations, which belong to ESA's space tracking station network (ESTRACK)
- The Mission Operations Centre (MOC), located at ESOC, Darmstadt, Germany
- The Science Operations Centre (SOC), located at ESAC, Villanueva de la Cañada, Spain
- The communications network, linking the various remotely located centres and stations to support the operational data traffic
The Science Operations Centre will be responsible for mission planning and the generation of payload operations requests to the MOC, as well as science data archiving. The SOC will be operational for the active science phase of the mission, i.e. from the beginning of the Cruise Phase onwards. The handover of payload operations from the MOC to the SOC is performed at the end of the Near-Earth Commissioning Phase (NECP). ESA's Malargüe ground station in Argentina will be used for all operations throughout the mission with the ground stations in New Norcia, Australia, and Cebreros, Spain, acting as backup when necessary.
During the initial cruise phase, which lasts until November 2021, Solar Orbiter will perform two gravity-assist manoeuvres around Venus and one around Earth to alter the spacecraft's trajectory, guiding it towards the innermost regions of the Solar System. At the same time, Solar Orbiter will acquire in situ data and characterise and calibrate its remote-sensing instruments. The first close solar pass will take place in 2022 at around a third of Earth's distance from the Sun.
The spacecraft's orbit has been chosen to be 'in resonance' with Venus, which means that it will return to the planet's vicinity every few orbits and can again use the planet's gravity to alter or tilt its orbit. Initially, Solar Orbiter will be confined to the same plane as the planets, but each encounter of Venus will increase its orbital inclination. For example, after the 2025 Venus encounter, it will make its first solar pass at 17° inclination, increasing to 33° during a proposed mission extension phase, bringing even more of the polar regions into direct view.
The spacecraft will make a close approach to the Sun every six months. The closest approach will be positioned to allow a repeated study of the same region of the solar atmosphere. Solar Orbiter will be able to observe the magnetic activity building up in the atmosphere that can lead to powerful solar flares or eruptions.
The objective of the mission is to perform close-up, high-resolution studies of the Sun and its inner heliosphere. The new understanding will help answer these questions:
- How and where do the solar wind plasma and magnetic field originate in the corona?
- 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?
The science payload is composed of 10 instruments:
- Heliospheric in-situ instruments (4)
- SWA - Solar Wind Plasma Analyser (United Kingdom): 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 characterizing 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)
- EPD - Energetic Particle Detector (Spain): To 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 (United Kingdom): It 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
- RPW - Radio and Plasma Wavesalyzer (France): Experience 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
- Solar remote-sensing instruments (6)
- PHI - Polarimetric and Helioseismic Imager (Germany): To 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 high-resolution and full-disk measurements of the photospheric magnetic field
- EUI - Extreme Ultraviolet Imager (Belgium): To 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. 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)
- SPICE - Spectral Imaging of the Coronal Environment (France): To 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 - Spectrometer Telescope for Imaging X-rays (Switzerland): To provide imaging spectroscopy of solar thermal and non-thermal X-ray emission from 4 to 150 keV. 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
- METIS (Multi Element Telescope for Imaging and Spectroscopy) - Coronagraph (Italy): To 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
- SolOHI - Solar Orbiter Heliospheric Imager (United States): To 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). (NRL provided)
Timeline and status
- April 2012: €300 million contract to build orbiter awarded to Astrium UK
- June 2014: Solar shield completes 2 week bake test
- September 2018: Spacecraft is shipped to IABG in Germany to begin the environmental test campaign
- February 2020: Successful launch
In April 2015, the launch was set back from July 2017 to October 2018. In August 2017, Solar Orbiter was considered "on track" for a launch in February 2019. The launch occurred on 10 February 2020 on an Atlas V 411.
The Atlas V 411 (AV-087) lifted off from SLC-41 at Cape Canaveral, Florida, at 04:03 UTC. The Solar Orbiter spacecraft separated from the Centaur upper stage nearly 53 minutes later, and the European Space Agency acquired the first signals from the spacecraft a few minutes later.
After launch, Solar Orbiter will take approximately 3.5 years, using repeated gravity assists from Earth and Venus, to reach its operational orbit, an elliptical orbit with perihelion 0.28 au and aphelion 0.91 au. The first flyby will be Venus in December 2020. Over the expected mission duration of 7 years, it will use additional gravity assists from Venus to raise its inclination from 0° to 25°, allowing it a better view of the Sun's poles. If an extended mission is approved, the inclination could rise further to 33°.
- Advanced Composition Explorer – NASA scientific satellite
- Parker Solar Probe – NASA robotic spacecraft to probe the outer corona of the Sun
- Solar Dynamics Observatory
- Solar and Heliospheric Observatory – European space observatory studying the Sun and its solar wind; cornerstone mission in the ESA Science Programme
- Solar Sentinels – A 2006 concept for a series of missions to the Sun
- Space sunshade – An spacecraft shield to reduce starlight and irradiation
- Ulysses – A 1990 solar orbiter
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