Trajectory design for a cislunar CubeSat leveraging dynamical systems techniques: The Lunar IceCube mission-Reference-Cited by-同舟云学术

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Trajectory design for a cislunar CubeSat leveraging dynamical systems techniques: The Lunar IceCube mission

Published:2018-03 Issue: Volume:144 Page:283-296
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Bosanac Natasha,Cox Andrew D.,Howell Kathleen C.,Folta David C.

Funder

NASA Goddard Space Flight Center

Busek

Catholic University of America

NASA

Purdue University's School of Aeronautics and Astronautics and College of Engineering

Zonta International Amelia Earhart Fellowship

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference26 articles.

1. Asteroid impact and deflection assessment mission;Cheng;Acta Astronaut.,2015

2. Lunar IceCube: determining volatile systematics via lunar orbiting cubesat;Clark;European Planetary Science Congress,2015

3. MarCO: interplanetary mission development on a CubeSat scale;Schoolcraft,2017

4. The Lunar IceCube mission design: construction of feasible transfer trajectories with a constrained departure;Folta,2016

5. The Lunar IceCube mission challenge: attaining science orbit parameters from a constrained approach trajectory;Folta,2017

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