Trajectory Maneuver Design of the NEA Scout Solar Sail Mission
收藏DataCite Commons2024-07-21 更新2025-04-16 收录
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http://dataverse.jpl.nasa.gov/citation?persistentId=doi:10.48577/jpl.IOKJTE
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The Near-Earth Asteroid Scout (NEA Scout) mission aimed to deliver a 6U CubeSat to a slow flyby of a Near Earth Asteroid using a solar sail as the primary propulsion system. NEA Scout was launched as a secondary payload aboard Artemis I, on 16 November 2022, but communication with the spacecraft was not achieved. This paper describes the target asteroid selection and the innovative trajectory and maneuver design for the NEA Scout mission, including cold gas maneuvers, multiple lunar flybys and solar sail thrusting. The resulting trajectory design tools, solutions, and analyses are potentially applicable to future solar sail missions.
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创建时间：
2024-07-21
