DSCOVR is built on the
SMEX-Lite spacecraft
bus and has a launch mass of approximately . The main science instrument sets are the Sun-observing Plasma Magnetometer (PlasMag) and the Earth-observing NIST Advanced Radiometer (NISTAR) and Earth Polychromatic Imaging Camera (EPIC). DSCOVR has two deployable solar arrays, a propulsion module, boom, and antenna. The propulsion module had 145 kg of
hydrazine propellant at launch. From its vantage point, DSCOVR monitors variable
solar wind conditions, provides early warning of approaching coronal mass ejections and observes phenomena on Earth, including changes in ozone, aerosols, dust and volcanic ash, cloud height, vegetation cover and climate. At its Sun-Earth location it has a continuous view of the Sun and of the sunlit side of the Earth. After the spacecraft arrived on-site and entered its operational phase, NASA began releasing near-real-time images of Earth through the EPIC instrument's website. The spacecraft is in a looping
halo orbit around the Sun–Earth
Lagrange point L1 in a six-month period, with a spacecraft–Earth–Sun angle varying from 4° to 15°.
Instruments PlasMag The Plasma-
Magnetometer (PlasMag) measures
solar wind for
space weather predictions. It can provide early warning detection of solar activity that could cause damage to existing satellite systems and ground infrastructure. Because solar particles reach about an hour before Earth, PlasMag can provide a warning of 15 to 60 minutes before a
coronal mass ejection (CME) arrives. It does this by measuring "the magnetic field and the velocity distribution functions of the electron, proton and alpha particles (
helium nuclei) of solar wind". • Magnetometer measures
magnetic field •
Faraday cup measures positively
charged particles • Electrostatic analyzer measures
electrons
EPIC away, centered on the
Americas. The Earth Polychromatic Imaging Camera (EPIC) takes images of the sunlit side of Earth for various Earth science monitoring purposes in ten different channels from
ultraviolet to
near-infrared.
Ozone and
aerosol levels are monitored along with cloud dynamics, properties of the land, and
vegetation. EPIC has an aperture diameter of , a
focal ratio of 9.38, a
field of view of 0.61°, and an angular sampling resolution of 1.07
arcseconds. Earth's
apparent diameter varies from 0.45° to 0.53° full width.
Exposure time for each of the 10 narrowband channels (317, 325, 340, 388, 443, 552, 680, 688, 764, and 779
nm) is about 40 ms. The camera produces 2048 × 2048 pixel images, but to increase the number of downloadable images to ten per hour the resolution is averaged to 1024 × 1024 on board. The final resolution is . Using NISTAR data, scientists can help determine the impact that humanity is having on the atmosphere of Earth and make the necessary changes to help balance the radiation budget. The radiometer measures in four channels: • For total radiation in
ultraviolet,
visible and
infrared in the range 0.2–100 μm • For reflected solar radiation in the ultraviolet, visible and near-infrared in the range 0.2–4 μm • For reflected solar radiation in infrared in the range 0.7–4 μm • For calibration purposes in the range 0.3–1 μm == Launch ==