Dragonfly Phase B Mission Design
收藏DataCite Commons2024-08-18 更新2025-04-16 收录
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http://dataverse.jpl.nasa.gov/citation?persistentId=doi:10.48577/jpl.MAVCRK
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The Dragonfly mission is designed to conduct a scientific survey of Titan with a relocatable lander and is enabled by a high-energy Delta-V Earth Gravity Assist (ΔV-EGA3+) trajectory. The trajectory utilizes a deep space maneuver, an Earth gravity assist, and a sequence of trajectory correction maneuvers, culminating in an entry, descent, and landing sequence. Several unique challenges exist when designing this trajectory, including accommodating a Multi-Mission Radioisotope Thermoelectric Generator and selecting a Titan atmospheric entry state. The current trajectory as of the Preliminary Design Review is described in detail, along with the trades and constraints that have influenced its design.
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Root
创建时间:
2024-08-18



