The Interstellar Mapping and Acceleration Probe (IMAP) is a heliophysics mission that simultaneously investigates 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. IMAP is a Sun-tracking spin-stabilized satellite in orbit about the Sun–Earth L1 Lagrange point with a science payload of ten instruments. IMAP also continuously broadcasts real-time in-situ data that can be used for space weather prediction. It is the fifth mission selected in the Solar Terrestrial Probes program, after TIMED, Hinode, STEREO and MMS. IMAP launched on 24 September 2025.
Science
Acceleration of charged particles up to high energy is ubiquitous throughout the universe, occurring at stars, magnetospheres, black holes, neutron stars, supernova remnants, and other locations. The precise processes behind this acceleration are not well understood. There are intermediate suprathermal particles which have energies between the energetic particles and the bulk thermal plasma. Understanding how these particles are energized and how they interact with the material within and beyond our solar neighborhood is one of the science topics that IMAP investigates. The solar wind and its associated magnetic field have blown a bubble in interstellar space called the heliosphere. IMAP studies the heliosphere boundary where the solar wind collides with material from the rest of the galaxy. Using Energetic Neutral Atoms (ENAs), IMAP images this interaction region from the inner Solar System. In addition, IMAP also directly measures the neutral particles of the interstellar medium, because they flow through the heliosphere relatively undisturbed. IMAP also investigates the source of the IBEX ribbon. IMAP's science goals are based on the four science objectives specified in the IMAP Announcement of Opportunity. IMAP will advance the understanding of:
The composition and properties of the local interstellar medium. How magnetic fields interact from the Sun through the local interstellar medium. How the solar wind and interstellar medium interact through the boundaries of our heliosphere. How particles are accelerated to high energies throughout the solar system.
Mission
Profile After launch, the spacecraft took several months to transit to about 1,500,000 km (930,000 mi) away from Earth towards the Sun at what is called the first Lagrange point (L1). The spacecraft then used on-board propulsion to insert into an +/−9.5° ×+/-3.9° Lissajous orbit around L1, very similar to the orbit of Advanced Composition Explorer (ACE). The baseline mission is 2 years, but all expendables are designed for a lifetime of more than 5 years.
Spacecraft
IMAP is a simple spin-stabilized (~4 RPM) spacecraft with ten instruments. Daily attitude maneuvers are used to keep the spin axis and top deck (with solar arrays) pointed in the direction of the incoming solar wind, which is a few degrees away from the Sun. In the L1 Lissajous orbit, the rear deck, with its communication antenna, approximately points at the Earth.
Instruments
The ten instruments on IMAP can be grouped into three categories: 1) Energetic neutral atom (ENA) detectors (IMAP-Lo, IMAP-Hi, and IMAP-Ultra); 2) Charged particle detectors (SWAPI, SWE, CoDICE, and HIT); and 3) Other coordinated measurements (MAG, IDEX, GLOWS). Shown here on the left are oxygen fluences measured at 1 AU by several instruments onboard Advanced Composition Explorer (ACE) during a 3-year period, with representative particle spectra obtained for gradual and impulsive Solar Energetic Particles (SEPs), corotating interaction regions (CIRs), anomalous cosmic rays (ACRs), and galactic cosmic rays (GCRs). The overlapping energy ranges for the various IMAP ion instrument measurements are indicated across the bottom. On the right, the panel shows characteristic energy distributions but for ENAs coming in from the heliosheath and VLISM; with the bottom also showing the overlapping energy ranges for the IMAP ENA instrument measurements and interstellar neutrals. Ion fluxes are from Voyager 1, along its particular trajectory and ENA Observations are from Cassini and IBEX for the same direction. Figure is adapted from McComas et al. 2018.
IMAP-Lo
IMAP-Lo is a single-pixel neutral atom imager, mounted on a pivot platform, that gives energy and angle-resolved measurements of ISN atoms (H, He, O, Ne, and D) tracked over >180° in ecliptic longitude and energy resolved global maps of ENA H and O. IMAP-Lo has heritage from the IBEX-Lo on IBEX but provides much larger collection power.
IMAP-Hi
IMAP-Hi consists of two identical, single-pixel high energy ENA Imagers that measure H, He, and heavier ENAs from the outer heliosphere. Each IMAP-Hi Imager is very similar in design to the IBEX-Hi ENA Imager but incorporate key modifications that enable substantially improved resolution, spectral range, and collection power. The instrument also incorporates a time-of-flight (TOF) system for identification of ENA species.
IMAP-Ultra
The IMAP-Ultra instrument images the emission of ENAs produced in the heliosheath and beyond, primarily in H atoms between ~3 and 300 keV, but it is also sensitive to contributions from He and O. Ultra is nearly identical to the Jupiter Energetic Neutral Imager (JENI), in development for flight on the European Space Agency's Jupiter Icy Moon Explorer (JUICE) mission to Jupiter and Ganymede. Ultra's primary differences from JENI are the use of two identical copies, one mounted perpendicular to the IMAP spin axis (Ultra90) and one mounted at 45° from the anti-sunward spin axis (Ultra45) for better sky coverage, and the use of slightly thicker, UV-filtering foils covering the back plane MCPs to reduce backgrounds associated with interstellar Lyman-α photons.
Solar Wind and Pick-up Ion (SWAPI)
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