API VERSION: 1.2 API SOURCE: NASA/JPL Horizons API ******************************************************************************* Revised: Mar 01, 2024 DART Spacecraft / Sun -135 https://dart.jhuapl.edu/ https://www.nasa.gov/planetarydefense/dart The Double Asteroid Redirect Test ("DART") is a NASA mission designed to demonstrate asteroid deflection by kinetic impact. The spacecraft launched on a SpaceX Falcon 9 rocket out of Vandenberg Space Force Base in California on 2021-Nov-24 @ 06:21:02 UTC. SEC01 was 10 minutes after launch. SECO2 was ~20 minutes after that. Spacecraft/booster separation at 07:17:20 UTC. BACKGROUND: DART's target is the binary asteroid system 65803 Didymos. Not on a path able to collide with Earth and presenting no hazard, the system is composed of two asteroids: the primary Didymos, and its smaller moonlet satellite asteroid, Dimorphos, which orbits Didymos at a distance of about 1.18 km every 11.92 hours. DART will autonomously navigate the last 4 hours to impact the moonlet Dimorphos nearly head-on in the fall of 2022, when ~11 million kilometers from Earth, shortening the time it takes to orbit the primary body Didymos by several minutes. Since the Didymos system is an eclipsing binary as viewed from Earth, Dimorphos passes in front of and behind Didymos, changing its brightness. Ground-based telescopes on Earth will be able to use this to assess the before/after effect caused by DART's impact at 6.6 km/s, producing data useful to "planetary defense" modeling. The LICIACube camera system will be deployed prior to impact and travel past the asteroid roughly three minutes after DART impacts to confirm the impact, document the spread of the resulting dust plume, attempt to capture an image of the newly formed crater and the opposite side of Dimorphos. KEY EVENT TIMES Launch: 24-Nov-2021 06:21:02 UTC Impact: 26-Sep-2022 23:14:24.183 UTC (actual) PHYSICAL CHARACTERISTICS: Main bus - box, dimensions ~ 1.2 x 1.3 x 1.3 meters, from which other structures extend to result in measurements of ~1.8 meters width, 1.9 meters length, 2.6 meters in height. - Two large solar panel arrays on each side, each 8.5 m long when deployed SCIENCE INSTRUMENTS: - DRACO: "Didymos Reconnaissance and Asteroid Camera for Optical navigation" A high-resolution imager derived from the New Horizons LORRI camera to support navigation and targeting, measure size and shape of the target, determine the impact site and geologic context. - LICIACube: "Light Italian Cubesat for Imaging of Asteroids" Deployed Sep. 12 UTC prior to the DART impact, LICIACube (6U) will capture images of the DART impact, resulting ejecta cloud, and potentially the impact crater on the surface of Dimorphos. TRAJECTORY: NOTE: Final reconstructed trajectory The mission-reconstructed DART trajectory can be used as an observing center (use '@' prefix ) OR as a target (drop the '@'). Related objects: @ -210 (LICIACube spacecraft) @ 20065803 (65803 Didymos system barycenter, pre-computed JPL s205) @ 920065803 (Didymos primary center, reconstructed JPL s547) @ 120065803 (Dimorphos, satellite of Didymos, reconstructed JPL s547) To instead numerically integrate the latest JPL ground-based solution for the Didymos system barycenter, request "65803;" (or select from menu list). The integrated database version can only be used as a target, not an observing center. Name Start (TDB) Stop (TDB) ------------------------------ ---------------------- ---------------------- dart_2021_328_2022_091_rec_v01 2021-Nov-24 07:17:53.0 2022-Apr-01 00:00:00.0 dart_2022_091_2022_231_rec_v01 2022-Apr-01 00:00:00.0 2022-Aug-19 00:01:09.2 dart_2022_231_2022_269_rec_v03 2022-Aug-19 00:01:09.2 2022-Sep-26 22:00:00.0 dart_2022_269_2022_269_rec_v03 2022-Sep-26 22:00:00.0 2022-Sep-26 23:14:45.3 dart_2022_269_2022_269_spc_v04 2022-Sep-26 23:14:45.3 2022 SEP 26 23:15:33.4 dart_2022_269_2099_001_imp_v03 2022-Sep-26 23:15:33.4 2099-Jan-01 00:00:99.0 *******************************************************************************