HIGH-ALTITUDE NEAR-CIRCULAR ORBITS FOR A LUNAR ORBITAL STATION

被引：0

作者：

Tselousova, Anastasia A. ^{[1
]}

Shirobokov, Maksim G. ^{[1
]}

Trofimov, Sergey P. ^{[1
]}

机构：

[1] Keldysh Inst Appl Math, 4 Miusskaya Sq, Moscow 125047, Russia

来源：

FIRST IAA/AAS SCITECH FORUM ON SPACE FLIGHT MECHANICS AND SPACE STRUCTURES AND MATERIALS | 2020年 / 170卷

基金：

俄罗斯科学基金会;

关键词：

ARTIFICIAL SATELLITES; PERTURBATIONS; EVOLUTION; PLANETS;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

High-altitude almost polar circular orbits around the Moon (10-15 thousand km above the surface) are currently proposed as a potential location of a prospective lunar orbital station. These orbits can be considered as an alternative to near-rectilinear halo orbits. The goal of this work is to compare geometrical and dynamical properties of various high-altitude circular obits and the resonant near-rectilinear halo orbits L2 9:2 and L2 4:1. To make a comparison, we investigate stability properties of the proposed orbits, eclipse conditions, and radio visibility of the lunar surface and station radio visibility from the Earth ground stations, including the Deep Space Network and stations located in Russia.

引用

页码：41 / 52

页数：12

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