Tethered spacecraft in asteroid gravitational environment-Reference-Cited by-同舟云学术

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Tethered spacecraft in asteroid gravitational environment

Published:2018-02 Issue: Volume:143 Page:126-132
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Burov Alexander A.,Guerman Anna D.,Kosenko Ivan I.,Nikonov Vasily I.

Funder

RFBR

EMaDeS

Centre for Mechanical and Aerospace Science and Technologies, C-MAST

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference43 articles.

1. To Space... by Electric Train;Artsutanov,1960

2. The orbital tower: a spacecraft launcher using the earth's rotational energy;Pearson;Acta Astronaut.,1975

3. Selected Papers;Zahnder,1978

4. The earth-to-moon highway;Artsutanov;Tech. Youth (Technika – Molodezhi),1979

5. Lunar anchored satellite test;Pearson,1978

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1. Modeling and stability analysis of a tethered asteroid probe system based on multi flexible body dynamics;Nonlinear Dynamics;2024-04-02

2. Linear stability analysis in tether system using its Hamiltonian function;The European Physical Journal Special Topics;2023-12

3. Dynamics and potential applications of a lunar space tethered system;Acta Astronautica;2020-04

4. Tension force in nanosatellite tethers systems;Journal of Physics: Conference Series;2019-10-01

5. Stationary configurations of space tether anchored on smaller primary in three-body problem;Acta Astronautica;2019-07

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