Optimal design of near-Earth asteroid sample-return trajectories in the Sun-Earth-Moon system

DOI10.1007/S10409-015-0527-1zbMath1361.70025OpenAlexW2205252026MaRDI QIDQ529216

Zhengfan Zhu, Chao Peng, Shengmao He, Yang Gao, Jian Ma, Xiao-Long Zhu

Publication date: 18 May 2017

Published in: Acta Mechanica Sinica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10409-015-0527-1

zbMATH Keywords

lunar gravity assistnear-Earth asteroidorbital resonancesample-return trajectoryspace trajectory design competition

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Cites Work

• Multiple Gravity Assists, Capture, and Escape in the Restricted Three-Body Problem

This page was built for publication: Optimal design of near-Earth asteroid sample-return trajectories in the Sun-Earth-Moon system