Mars gravity assist to improve missions towards main-belt asteroids

Author:

Casalino Lorenzo,Colasurdo Guido

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference7 articles.

1. The Year in Review: Electric Propulsion;Ho;Aerospace America,2001

2. Optimal Low-Thrust Escape Trajectories Using Gravity Assist;Casalino;Journal of Guidance, Control, and Dynamics,1999

3. Optimization Procedure for Preliminary Design of Opposition-Class Mars Missions;Casalino;Journal of Guidance, Control, and Dynamics,1998

4. Optimization of ΔV Earth-Gravity-Assist Trajectories;Casalino;Journal of Guidance, Control, and Dynamics,1998

5. Trajectories towards Near-Earth Objects Using Solar Electric Propulsion;Colasurdo;Paper AAS 99-339,1999

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Optimization of Variable-Specific-Impulse Gravity-Assist Trajectories;Journal of Spacecraft and Rockets;2020-03

2. Low-energy near Earth asteroid capture using Earth flybys and aerobraking;Advances in Space Research;2018-04

3. Mission Analysis for Sample Retrieval from a Primitive Near-Earth Asteroid;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN;2009

4. Improved Edelbaum's Approach to Optimize Low Earth/Geostationary Orbits Low-Thrust Transfers;Journal of Guidance, Control, and Dynamics;2007-09

5. Improved Edelbaum's Approach to Optimize LEO-GEO Low-Thrust Transfers;AIAA/AAS Astrodynamics Specialist Conference and Exhibit;2004-06-22

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