Novel orbits of Mercury, Venus and Mars enabled using low-thrust propulsion-Reference-Cited by-同舟云学术

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Novel orbits of Mercury, Venus and Mars enabled using low-thrust propulsion

Published:2014-02 Issue:2 Volume:94 Page:634-645
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Anderson Pamela,Macdonald Malcolm,Yen Chen-wan

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference23 articles.

1. 2001 Mars Odyssey Aerobraking;Smith;J. Spacecr. Rockets,2005

2. The Mars Express Mission: an Overview.;Chicarro,2004

3. An overview of the Mars Reconnaissance Orbiter (MRO) science mission;Zurek;J. Geophys. Res.,2006

4. A Vision for the Exploration of Mars: Robotic Precursors Followed by Humans to Mars Orbit in 2033;Sellers,2012

5. S. Squyres, Vision and Voyages For Planetary Science in the Decade 2013–2022, 2011.

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1. 3- and 6-degree-of-freedom analysis of the Magellan aerobraking experiment and planar aerobraking at Venus;Aerospace Science and Technology;2024-09

2. Sun–Venus CR3BP, part 1: periodic orbit generation, stability, and mission investigation;Archive of Applied Mechanics;2024-03-01

3. Sun–Venus CR3BP, part 2: resonance investigation and planar periodic orbit family generation;Archive of Applied Mechanics;2024-02-08

4. Trajectory approximation of a passively actuated solar balloon in near-Earth mission scenarios;Acta Astronautica;2021-11

5. Mission Design for the 2020 Mercury Lander Decadal Survey;The Journal of the Astronautical Sciences;2021-09-02

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