ESA Vigil

Last updated
Vigil
ESA Vigil mission patch.png
NamesFormerly known as Lagrange
Mission typeSpace Weather nowcast/forecast
Operator European Space Agency
COSPAR ID TBD
SATCAT no. TBD
Website https://www.esa.int/Space_Safety/Vigil
Mission durationCruise phase: 3 years

Operations: 4.5 years

Extension: up to 5 years
Spacecraft properties
Launch mass2,500 kg (limit)
Dry mass~1,100 kg
Payload mass~150 kg (before system margins)
PowerSpacecraft ~1000 W; Payload ~200 W
Start of mission
Launch date2031 (planned) [1]
Rocket Ariane 62
Launch site Guiana Space Centre
Contractor Arianespace
Orbital parameters
Reference systemSun-Earth L5
RegimeLissajous orbit

Vigil, [2] formerly known as Lagrange, [3] is a space weather mission developed by the European Space Agency. The mission will provide the ESA Space Weather Office with instruments able to monitor the Sun, its solar corona and interplanetary medium between the Sun and Earth, to provide early warnings of increased solar activity, to identify and mitigate potential threats to society and ground, airborne and space based infrastructure as well as to allow 4 to 5 days space weather forecasts. [4] To this purpose the Vigil mission will place for the first time a spacecraft at Sun-Earth Lagrange point 5 (L5) from where it would get a 'side' view of the Sun, observing regions of solar activity on the solar surface before they turn and face Earth.

Contents

Monitoring space weather includes events such as solar flares, coronal mass ejections, geomagnetic storms, solar proton events, etc. [5] The Sun-Earth L5 location provides opportunities for space weather forecasting by monitoring the Sun beyond the Eastern solar limb not visible from Earth, thus increasing the forecast lead time of potentially hazardous solar phenomena including solar flares, fast solar wind streams.

The Vigil mission will improve the assessment of Coronal Mass Ejection (CME) motion and density, speed/energy, arrival time and impact on Earth to support protection of the critical infrastructure on ground and in space. The mission will also perform in-situ observations of the solar wind bulk velocity, density, and temperature as well as the Interplanetary magnetic field(IMF) at L5, to provide enhanced detection and forecasting of high-speed solar wind streams and co-rotating interaction regions.

Status

As part of the Space Situational Awareness Programme (SSA), [6] ESA initiated in 2015 the assessment of two missions to enhance space weather monitoring. These missions were initially meant to utilize the positioning of satellites at the Sun-Earth Lagrangian L1 and L5 points.

Eventually, in the frame of the cooperation on space-based space weather observations between the European Space Agency (ESA) and the United States National Oceanic and Atmospheric Administration (NOAA) National Environmental Satellite Data and Information Service (NESDIS) the following was agreed[ citation needed ]:

In the scope of this agreement the two agencies will share data and provide each other with instruments to be embarked on the respective platforms.

The space segment of the Vigil mission completed the first part of Preliminary Definition (Phase B1) [7] in June 2022. On 21 November 2022, ESA issued a Request for Quotation to Airbus Defence and Space Ltd. for the design, development and verification (Phase B2, C and D) of the Vigil Space Segment. [8] The formal start of the activities is planned before the end of 2023.

The status of the Ground Segment is ... [to be completed].

Vigil is scheduled to be launched in 2031, [1] followed by 3 years of cruise to L5. The mission aims to operate nominally for 4.5 years, with a possibility of extension up to 5 additional years.

Objectives

Vigil mission objectives can be grouped in two main categories:

Mission Architecture

Space Segment

Platform

The Platform supplies all service-related functions required to support the proper operation and data collection of the Vigil Payload Suite. The key feature of spacecraft concept for an operational mission like Vigil is a robust avionics architecture able to remain operational during the most extreme space weather events seen in the last 100 years. The Failure Detection Isolation and Recover (FDIR) will be designed to enhance the autonomy of the spacecraft, thus reducing the risk of service interruption requiring ground intervention.

The Mission Data downlink is via X-band at an average data rate of ~1 Mbps (~86 Gbits per day) with 24/7 coverage provided by ESTRACK supplemented by additional commercial stations.

The mass at launch is projected close to 2500 kg. To reach SEL5 the proposed design will rely on a bi-propellant Chemical Propulsion System equipped with a 450 N main engine.

Payload Suite

Payload Suite will include:

  • 3 remote sensing instruments;
  • 2 in-situ instruments;

In the frame of the inter-agency cooperation between ESA and NASA, Vigil will offer the possibility to accommodate an additional instrument NASA instrument of opportunity (NIO). [9]

Remote sensing instruments

The remote sensing instruments will allow to estimate size, mass, speed, and direction of CMEs.

  • Compact Coronagraph (CCOR): it will image the solar corona and be used to observe Coronal Mass Ejections (CMEs). With CCOR data the size, mass, speed, and direction of CMEs can be derived. The CCOR Instrument will be provided to ESA by NOAA and manufactured by U.S. Naval Research Laboratory (NRL). The design will instrument is based on the heritage of a similar instrument for NOAA's mission SWFO-1 and GOES-U. [10]
  • Heliospheric Imager (HI): it will provide wide-angle, white-light images of the region of space between the Sun and the Earth (i.e., the heliosphere). These images are required to enable tracking of Earth-directed CMEs over their propagation path once they have left the field-of-view of the coronagraph instrument.
  • Photospheric Magnetic field Imager (PMI): it will scan a selected solar spectrum to generate 3D maps of the magnetic field (field strength, azimuth, inclination) and crucial physical parameters (e.g. distribution of vertical and horizontal magnetic fields, distribution of inclination angles, twist, writhe, helicity, current density, share angles, photospheric magnetic excess energy etc.) for enhanced space weather applications. The instrument will also generate solar white light images as by-products of magnetograph measurements and produced as continuum images observed at an additional wavelength point in the vicinity of the magnetically sensitive spectral line.
In-situ instruments

In-situ instruments can be used to monitor the Stream Interaction Regions (SIR) [11] and Co-rotating Interaction Regions (CIR) up to 4–5 days in advance before their arrival at Earth.

  • Plasma Analyser (PLA): it will measure Solar wind bulk velocity, solar wind bulk density and solar wind temperature, are required for monitoring of the solar wind that is turning towards the Earth and particularly for detection of high-speed solar wind streams that produce Stream Interaction Regions (SIR) and Co-rotating Interaction Regions (CIR).
  • Magnetometer (MAG): it will measurement of the Interplanetary Magnetic Field (IMF) at L5; to minimise the effects of the electromagnetic interferences generated by the Vigil spacecraft itself, the MAG will be placed at the end of a 7m boom.
Institutions involved

Pictogram voting wait.svg  Pending

Ground Segment

The Ground Segment, consists of:

Launcher

The Launcher service is baselined as Ariane 6.2 by Arianespace from the Guiana Space Centre. The launcher will be in dual-launch configuration for injection in GTO. The Spacecraft will be launched as secondary passenger with a commercial customer bound for geostationary orbit in a dual-launch with Ariane 6.4. This transfer option makes use of the Sun-Earth L1/L2 connection and the Weak Stability Boundary effects near L2 to reach L5.

After release of the Spacecraft into GTO, it will perform a series of 3 Apogee Raising Manoeuvres (ARM) to make its way towards L1 within a period of 14 days, planned to minimise the transitions through the Van Allen belts.

From L1 the Spacecraft will be placed on a zero to low-cost transfer trajectory towards L2 from which it will then leave towards SEL5. Deep Space Manoeuvres (DSM), preceded and followed by correction manoeuvres, will be executed as needed.

When the Spacecraft reaches L5, a braking manoeuvre to insert the spacecraft into the final orbit will be executed. Different options are investigated, resulting in a split of such manoeuvre in two burns.

The cruise to L5 can take up to 3 years. To increase the use of the Vigil spacecraft, the mission will enter in a pre-operational phase once the halfway through the journey L5.

Alternatives include the use of Ariane 6.2 for direct injection in SEL5, Ariane 6.4 or Falcon 9 provided by SpaceX.

Related Research Articles

<span class="mw-page-title-main">Lagrange point</span> Equilibrium points near two orbiting bodies

In celestial mechanics, the Lagrange points are points of equilibrium for small-mass objects under the gravitational influence of two massive orbiting bodies. Mathematically, this involves the solution of the restricted three-body problem.

<span class="mw-page-title-main">Solar wind</span> Stream of charged particles from the Sun

The solar wind is a stream of charged particles released from the Sun's outermost atmospheric layer, the corona. This plasma mostly consists of electrons, protons and alpha particles with kinetic energy between 0.5 and 10 keV. The composition of the solar wind plasma also includes a mixture of particle species found in the solar plasma: trace amounts of heavy ions and atomic nuclei of elements such as carbon, nitrogen, oxygen, neon, magnesium, silicon, sulfur, and iron. There are also rarer traces of some other nuclei and isotopes such as phosphorus, titanium, chromium, and nickel's isotopes 58Ni, 60Ni, and 62Ni. Superimposed with the solar-wind plasma is the interplanetary magnetic field. The solar wind varies in density, temperature and speed over time and over solar latitude and longitude. Its particles can escape the Sun's gravity because of their high energy resulting from the high temperature of the corona, which in turn is a result of the coronal magnetic field. The boundary separating the corona from the solar wind is called the Alfvén surface.

<i>Ulysses</i> (spacecraft) 1990 robotic space probe; studied the Sun from a near-polar orbit

Ulysses was a robotic space probe whose primary mission was to orbit the Sun and study it at all latitudes. It was launched in 1990 and made three "fast latitude scans" of the Sun in 1994/1995, 2000/2001, and 2007/2008. In addition, the probe studied several comets. Ulysses was a joint venture of the European Space Agency (ESA) and the United States' National Aeronautics and Space Administration (NASA), under leadership of ESA with participation from Canada's National Research Council. The last day for mission operations on Ulysses was 30 June 2009.

<span class="mw-page-title-main">Space weather</span> Branch of space physics and aeronomy

Space weather is a branch of space physics and aeronomy, or heliophysics, concerned with the varying conditions within the Solar System and its heliosphere. This includes the effects of the solar wind, especially on the Earth's magnetosphere, ionosphere, thermosphere, and exosphere. Though physically distinct, space weather is analogous to the terrestrial weather of Earth's atmosphere. The term "space weather" was first used in the 1950s and popularized in the 1990s. Later, it prompted research into "space climate", the large-scale and long-term patterns of space weather.

<span class="mw-page-title-main">Coronal mass ejection</span> Ejecta from the Suns corona

A coronal mass ejection (CME) is a significant ejection of magnetic field and accompanying plasma mass from the Sun's corona into the heliosphere. CMEs are often associated with solar flares and other forms of solar activity, but a broadly accepted theoretical understanding of these relationships has not been established.

<span class="mw-page-title-main">Solar and Heliospheric Observatory</span> European space observatory

The Solar and Heliospheric Observatory (SOHO) is a European Space Agency (ESA) spacecraft built by a European industrial consortium led by Matra Marconi Space that was launched on a Lockheed Martin Atlas IIAS launch vehicle on 2 December 1995, to study the Sun. It has also discovered over 5,000 comets. It began normal operations in May 1996. It is a joint project between the European Space Agency (ESA) and NASA. SOHO was part of the International Solar Terrestrial Physics Program (ISTP). Originally planned as a two-year mission, SOHO continues to operate after over 25 years in space; the mission has been extended until the end of 2025, subject to review and confirmation by ESA's Science Programme Committee.

<span class="mw-page-title-main">Deep Space Climate Observatory</span> American solar research spacecraft

Deep Space Climate Observatory is a National Oceanic and Atmospheric Administration (NOAA) space weather, space climate, and Earth observation satellite. It was launched by SpaceX on a Falcon 9 v1.1 launch vehicle on 11 February 2015, from Cape Canaveral. This is NOAA's first operational deep space satellite and became its primary system of warning Earth in the event of solar magnetic storms.

<span class="mw-page-title-main">Advanced Composition Explorer</span> NASA satellite of the Explorer program

Advanced Composition Explorer is a NASA Explorer program satellite and space exploration mission to study matter comprising energetic particles from the solar wind, the interplanetary medium, and other sources.

<span class="mw-page-title-main">Solar Orbiter</span> European space-based solar observatory

The Solar Orbiter (SolO) is a Sun-observing probe developed by the European Space Agency (ESA) with a National Aeronautics and Space Administration (NASA) contribution. Solar Orbiter, designed to obtain detailed measurements of the inner heliosphere and the nascent solar wind, will also perform close observations of the polar regions of the Sun which is difficult to do from Earth. These observations are important in investigating how the Sun creates and controls its heliosphere.

<span class="mw-page-title-main">STEREO</span> Solar observation mission (2006–present)

STEREO is a solar observation mission. Two nearly identical spacecraft were launched in 2006 into orbits around the Sun that cause them to respectively pull farther ahead of and fall gradually behind the Earth. This enabled stereoscopic imaging of the Sun and solar phenomena, such as coronal mass ejections.

The Solar Sentinels was a series of proposed space missions to the Sun. Solar Sentinels was proposed in 2006 in conjunction with other Sun missions, and another simpler proposal was submitted in 2008.

<span class="mw-page-title-main">Aditya-L1</span> Indias first solar observation mission

Aditya-L1 is a coronagraphy spacecraft for studying the solar atmosphere, designed and developed by the Indian Space Research Organisation (ISRO) and various other Indian Space Research Institutes. It is orbiting at about 1.5 million km from Earth in a halo orbit around the Lagrange point 1 (L1) between the Earth and the Sun, where it will study the solar atmosphere, solar magnetic storms, and their impact on the environment around the Earth.

<span class="mw-page-title-main">Heliophysics Science Division</span>

The Heliophysics Science Division of the Goddard Space Flight Center (NASA) conducts research on the Sun, its extended Solar System environment, and interactions of Earth, other planets, small bodies, and interstellar gas with the heliosphere. Division research also encompasses geospace—Earth's uppermost atmosphere, the ionosphere, and the magnetosphere—and the changing environmental conditions throughout the coupled heliosphere.

<span class="mw-page-title-main">July 2012 solar storm</span> Notable coronal mass ejection

The solar storm of 2012 was a solar storm involving an unusually large and strong coronal mass ejection that occurred on July 23, 2012. It missed Earth with a margin of approximately nine days, as the equator of the Sun rotates around its own axis with a period of about 25 days.

<span class="mw-page-title-main">Solar phenomena</span> Natural phenomena within the Suns atmosphere

Solar phenomena are natural phenomena which occur within the atmosphere of the Sun. They take many forms, including solar wind, radio wave flux, solar flares, coronal mass ejections, coronal heating and sunspots.

<span class="mw-page-title-main">GOES-19</span> NOAA weather satellite

GOES-19 is a weather satellite, the fourth and last of the GOES-R series of satellites operated by the National Oceanic and Atmospheric Administration (NOAA). The GOES-R series will extend the availability of the Geostationary Operational Environmental Satellite (GOES) system until 2036. The satellite is built by Lockheed Martin, based on the A2100 platform.

<span class="mw-page-title-main">Interstellar Mapping and Acceleration Probe</span> Planned NASA heliophysics mission

The Interstellar Mapping and Acceleration Probe(IMAP) is a heliophysics mission that will simultaneously investigate two important and coupled science topics in the heliosphere: the acceleration of energetic particles and interaction of the solar wind with the local interstellar medium. These science topics are coupled because particles accelerated in the inner heliosphere play crucial roles in the outer heliospheric interaction. In 2018, NASA selected a team led by David J. McComas of Princeton University to implement the mission, which is currently scheduled to launch on 29 April 2025. IMAP will be a Sun-tracking spin-stabilized satellite in orbit about the Sun–Earth L1 Lagrange point with a science payload of ten instruments. IMAP will also continuously broadcast real-time in-situ data that can be used for space weather prediction.

Polarimeter to Unify the Corona and Heliosphere (PUNCH) is a future mission by NASA to study the unexplored region from the middle of the solar corona out to 1 AU from the Sun. PUNCH will consist of a constellation of four microsatellites that through continuous 3D deep-field imaging, will observe the corona and heliosphere as elements of a single, connected system. The four microsatellites were initially scheduled to be launched in October 2023, but they have since been moved to a launch in rideshare with SPHEREx, scheduled for 27 February 2025.

<span class="mw-page-title-main">Space Weather Follow On-Lagrange 1</span> Planned spacecraft mission

Space Weather Follow On-Lagrange 1 (SWFO-L1) is a future spacecraft mission planned to monitor signs of solar storms, which may pose harm to Earth's telecommunication network. The spacecraft will be operated by the National Oceanic and Atmospheric Administration (NOAA), with launch scheduled for 29 April 2025. It is planned to be placed at the Sun–Earth L1 Lagrange point, a location between the Earth and the Sun. This will allow SWFO-L1 to continuously watch the solar wind and energetic particles heading for Earth. SWFO-L1 is an ESPA Class Spacecraft, sized for launch on an Evolved Expendable Launch Vehicle Secondary Payload Adapter (ESPA) Grande ring in addition to the rocket's primary payload. The spacecraft's Solar Wind Instrument Suite (SWIS) which includes three instruments will monitor solar wind, and the Compact Coronagraph (CCOR) will monitor the Sun's surroundings to image coronal mass ejection (CME). A CME is a large outburst of plasma sent from the Sun towards interplanetary space.

References

  1. 1 2 Foust, Jeff (23 May 2024). "Airbus to build ESA space science satellite". SpaceNews . Retrieved 23 May 2024.
  2. "Introducing: ESA Vigil". www.esa.int. Retrieved 2023-06-19.
  3. "The "no name" space weather mission". www.esa.int. Retrieved 2023-06-19.
  4. Kraft, S.; Luntama, J. P.; Puschmann, K. G. (2017-09-25). "Remote sensing optical instrumentation for enhanced space weather monitoring from the L1 and L5 Lagrange points". In Karafolas, Nikos; Cugny, Bruno; Sodnik, Zoran (eds.). International Conference on Space Optics — ICSO 2016. SPIE. p. 81. doi:10.1117/12.2296100. ISBN   978-1-5106-1613-4. S2CID   134935417.
  5. Monitoring space weather. European Space Agency (ESA). 4 December 2017.
  6. "SSA Programme overview". www.esa.int. Retrieved 2023-06-19.
  7. "How a mission is chosen". www.esa.int. Retrieved 2023-06-19.
  8. "esa-star Doing". doing-business.sso.esa.int. Retrieved 2023-06-19.
  9. "Vigil Focused Mission of Opportunity (FMO) under the Living With a Star Program". lws.larc.nasa.gov. Retrieved 2023-06-19.
  10. "Compact Coronagraph (CCOR)". National Environmental Satellite, Data, and Information Service. Retrieved 2023-06-19.
  11. Richardson, Ian G. (2018). "Solar wind stream interaction regions throughout the heliosphere". Living Reviews in Solar Physics. 15 (1): 1. Bibcode:2018LRSP...15....1R. doi:10.1007/s41116-017-0011-z. PMC   6390897 . PMID   30872980.